I-2 - University of Cincinnatiprogram/program/ABET_I-2_syllabi.doc · Web viewEngineering Fundamentals Course Syllabi I-2 Page 44 Appendix I-2.1. Aerospace Engineering Course Syllabi

Appendix I-2.Appendix I-2.1. Aerospace Engineering Course Syllabi.......................I-2 Page 2

Appendix I-2.2. Engineering Fundamentals Course Syllabi..............I-2 Page 44

UNIVERSITY OF CINCINNATI AEROSPACE ENGINEERING JUNE 2004

Appendix I-2.1. Aerospace

Engineering Course Syllabi

Appendix I-2 Page I-2.2


AEEM-100 Introduction to Aerospace Engineering Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-100. Introduction to Aerospace Engineering. 1 cr. Introduction to college staff and organizations. Small group work, including ethics, the co-op program, and a team project in creative problem solving

Prerequisites: None.Textbook: Creative Problem Solving: Thinking Skills for a Changing World, E. Lumsdane

and M. Lumsdane, McGraw-Hill, 1995References: None.Coordinator: Paul Orkwis, Associate Professor of Aerospace Engineering & Engineering

Mechanics, 478 ERC, 556-3366, [email protected] Objectives: The student will be able to

1. Understand the mission of the AsE & EM Department and College of Engineering, the services they offer, and the location of all Departmental, College and University facilities. 2. Study skills and time management necessary for success in engineering, mathematics, and basic sciences. 3. Recognize how freshman year basic science courses form the basis of later engineering fundamentals courses and departmental courses. This is achieved through an introduction to aerodynamics, propulsion, structures, dynamics and controls, and space systems4. Learn about the nature of co-op jobs and co-op employment. 5. Describe engineering practice and the work involved in the profession; develop a sense of ethical behavior as applied to engineering practice. [f]6. Fabricate a rectangular wing and subsequently test it in wind tunnel [i, j, k]7. Prepare overall project report [g]

Topics Covered: Aerospace Curriculum, Faculty and Staff, time management, study skills, introduction to aerodynamics, propulsion, structures, and control and space systems, application of current courses, description of engineering practice, ethics, and co-op program.

Computer usage:Professional Experience:

Engineering; General Education

AEEM Program Objectives:

3, 4, 5, and 6

ABET Criteria Addressed:

An appreciation of an engineer’s professional and ethical responsibilities [f]

An ability to study effectively An ability to work on a team and communicate effectively [g] An ability to use wind tunnel for lift and drag measurements [k] Elementary ability to fabricate a composite wing [i, j] An ability to write a report of their findings [g]

AEEM 110 Introduction to Aircraft Engineering Date Prepared: February 2, 2004

Catalog data: 20-AEEM-110. Introduction to Aircraft Engineering. 1 cr. History of Aviation. Topical case studies from trade/technical publications. Aeronautical



terminology. Role of disciplines and their interrelations. Role and importance of basic sciences and mathematics. Design, fabricate, and test a flying wing.

Prerequisites: 20-AEEM-100 Introduction to Aerospace Engineering.Textbook: Introduction to Flight, J.D.Anderson, McGraw HillReferences: Aviation Week and Space TechnologyCoordinator: Shaaban Abdallah, Professor of Aerospace Engineering & Engineering

Mechanics, 721 Rhodes, 556-3321, [email protected] Objectives: The student will be able to

1. Recall the basic history and current issues in Aviation and the contribution of Aerospace Engineering [j] 2. Define basic aeronautical terminology and describe the particular subsystems3. Define the basic disciplines inherent in aerospace engineering and their interconnectivity [j]4. Recognize how freshman year basic science courses form the basis of later engineering fundamental and departmental courses 5. Utilitze MATLAB to solve simple problems [k]6. Design, fabricate, and test a radio-controlled ZAGI™ wing, [c]7. Write a short report for the ZAGI™ wing. [g]

Topics Covered: History of aviation, the role of technical societies, topical case studies from current trade/technical periodicals to explore: aeronautical terminology and subsystems, aerospace disciplinary roles, interdisciplinary cooperation.

Computerusage:

CompuFoil™ for wing design; MATLAB

Professional Experience:

Engineering; General Education; Design Experience


3, 4, 5, and 6


An ability to design, fabricate, and test a wing [c, k] An ability to work with a team and communicate effectively [g] A knowledge of contemporary and historical issues [j]



AEEM 111 Introduction to Spacecraft Engineering Date prepared: April 21, 2004

Catalog data: 20-AEEM-111. Introduction to Spacecraft Engineering. 1 cr. Development of the fundamental concepts of spaceflight mechanics. Applications to Earth orbiting spacecraft.

Prerequisites: 20-AEEM-100 Introduction to Aerospace Engineering.Textbook: (Recommended) Understanding Space: An Introduction to Aeronautics, J.J. Sellers,

McGraw-Hill Space Technology Series, 2004 (revised 2nd ed.)References: None.Coordinator: Trevor Williams, Professor of Aerospace Engineering & Engineering Mechanics,

735 Rhodes, 556-3221, [email protected] Objectives: The student will be able to

1. Basic Orbital Mechanics Newton’s laws, inverse square law of gravitation, Kepler’s laws [a] Two-body problem; orbital period as a function of orbit geometry; orbital

elements [a] Conservation of energy; speed vs. altitude; Kepler’s equation [a] Sensitivity of orbit to initial velocity errors; practical implications for orbit

insertion [a] Relative orbital motion: rendezvous/docking missions [a] Introduction to in-plane and out-of-plane maneuvers; launch windows [a] Satellite ToolKit (STK) exercise: orbital ground tracks and Earth coverage. [k,

g]2. Fundamentals of Spacecraft Engineering Practical satellite roles: e.g. Earth observation, communications, astronomy,

navigation [h, j] The space environment: vacuum; microgravity; thermal extremes; radiation [a] Implications of space environmental effects on spacecraft design and

implications of launch loads on spacecraft structural design [c] Introduction to spacecraft hardware for attitude control (e.g. wheels,

magtorquers, thrusters, gyros, GPS) [e] Introduction to spacecraft power generation hardware (e.g. solar cells, fuel

cells, batteries, RTGs) [e] Spacecraft design trade-offs: e.g. communications power vs. antenna gain and

pointing; orbital architecture [c] Spacecraft design case studies: Apollo mode decision, Mars landers, Hubble [c,

j]3. Hands-on project Construction of CricketSats (small sensor package analogous to those in small

spacecraft) in teams of five students each [b, c, d] Functional testing and calibration of CricketSats [b, d] Drop-testing of protected CricketSats (analogous to airbag touchdown of Mars

landers) [c, d]Topics Covered: The three main topics covered by this course are: basic orbital mechanics (including

use of Satellite ToolKit orbital analysis software), fundamentals of spacecraft engineering, and a hands-on project. Specifically this will include Newton’s Laws, Kepler’s Laws, the environment of space, two-body motion, orbital motion period, speed, distance, and position, Kepler’s equation, Hohmann transfers, the rocket equation, & the rendezvous equations.

Computer usage: Satellite ToolKitProfessional Experience:

Mathematics; Engineering

AEEM Program 1 through 6



Objectives:ABET Criteria Addressed:

Will have a basic understanding of orbital mechanics [a] Will have a basic understanding of spacecraft engineering principles [a, c] Will have experience building & calibrating an electronic circuit [b] Will have experience working in teams on a hands-on design project [c, d, k] Will have elementary skills in STK orbits analysis package [k] Will have the ability to write a report presenting their design [g] Will have an understanding of the uses and impact of spacecraft in society [h, j]



AEEM 211 Basic Integrated Engineering Date Prepared: February 2, 2004

Catalog data: 20-AEEM-211. Basic Integrated Engineering. 3 cr. Elementary design concepts, team problem solving, optimization of fundamental engineering problems, and oral and written communication skills

Prerequisites: 20-ENFD-111 Computer Language; 20-ENFD-101 Mechanics I; 15-MATH-253 Calculus III; 15-PHYS-201 Physics I

Textbook: None.References: Applied Optimal Design, Haug, E.J. and Arora, J.S., Wiley, NY

The Engineering Design Process, Ertas, E. and Jones, J.C., Wiley, NYCoordinator: Paul Orkwis, Associate Professor of Aerospace Engineering & Engineering

Mechanics, 478 ERC, 556-3366, [email protected] Objectives: The student will be able to

1. Describe the relationship between general design theory principles, the Hermann four-quadrant brain model, creative problem solving mindsets and concurrent engineering [h, k]

2. Solve practical engineering problems with non-unique solutions using calculus, physics, statics and a computer language [a, b, c, e, i, j]

3. Work in a team to solve problems [d, f]4. Write technical reports [g]5. Deliver oral presentations [g]6. Apply elementary optimization methods to perform trade-off studies for a

simple design governed by statics.Topics Covered: Creative problem solving techniques, brainstorming, brain models, general

theory of design, concurrent engineering, technical writing, oral presentation, optimization, cost functions, constraints.

Computerusage:Professional Experience:

Mathematics; Engineering; General Education; Design Experience


1, 2, 3, 4 and 6


Know how to apply the knowledge of calculus, computer science, physics, and mechanics to solve engineering problems [a, b, f, h, i, j, k]

Be able to design a simple system and optimize it [c, e, g, i, j] Be able to work in a team environment [d, g] Be able to present the design in the form of an oral presentation and written

report [g]



AEEM 212 Probabilistic Engineering Date prepared: Feb 2, 2004

Catalog data: 20-AEEM-212. Probabilistic Engineering. 3 cr. Probability and statistics for design and reliability, design case studies, and continuation of engineering design experience from Basic Integrated Engineering

Prerequisites: 20-AEEM-211 Basic Integrated Engineering; 15-MATH-254 Calculus IVTextbook: Statistical Method for Engineers, G.G. Vining, Duxbury, 1998References: Applied Statistics for Engineers and Scientists, J. Devore & N. Farnum, Duxbury,

1998Coordinator: Bruce K. Walker, Associate Professor of Aerospace Engineering & Engineering

Mechanics, 745B Baldwin, 556-3552, [email protected] Objectives:

The student will be able to

1. Construct and interpret representations of random data including histograms, relative frequency tables, and box plots [b]

2. Compute mean, median, variance, standard deviation and quartiles from random data [a, b]

3. Conduct a lab experiment and evaluate the data for variables [b]4. Construct probabilities of composite events from independent and elementary

events [a, b]5. Use and interpret probability mass functions and probability density

functions, including calculation of mean and variance [a, b]6. Use the standard normal distribution to compute probabilities for ranges of

values and for constructing confidence intervals [a, b]7. Compute and interpret correlation coefficients for jointly distributed random

variables [a, b]8. Calculate statistics of linear combinations of random quantities, as used in

meeting tolerance specifications [a, e, k]9. Construct and interpret simple control charts (mean chart and range chart) for

statistical process control and process capability analysis [e, k]10. Analyze the reliability of simple systems involving parallel and series

subsystems, including computation of reliability and comparison of reliabilities using more or less reliable components [a, e, h, k]

11. Solve design problems involving quantities (strength, dimensions, etc.) that include random variations with variances given [c]

12. Appreciate the importance of six sigma concepts in manufacturing & design process [i, j, k]

13. Write technical reports [g]Topics Covered: Data representation for random data. Sample statistics. Basic properties of

probabilities. Events and event probabilities and independent and mutually exclusive events. Random variables and probability mass functions, probability density functions, and cumulative distribution functions. Expectation and mean and variance. Binomial, Poisson, hypergeometric, uniform, normal, exponential, & Weibull distributions. Jointly distributed random variables and correlation. Functions of random variables including linear combinations. Tolerances. Error and variation of computed sample statistics. Control charts and process capability. Reliability.


Mathematics; Engineering; General Education; Design Experience

AEEM Objectives:

1, 2, 3, 4 and 6

ABET Criteria Know how to apply statistical tools to interpret large amounts of random data



Addressed: from homework and projects [a] Be able to conduct an experiment and analyze & interpret the data for

variability [b] Be able to apply probabilistic concepts to simple design problems [c] Be able to design components to meet tolerance specifications [e] Be able to write a technical report [g] Be able to improve quality and reliability of product [h] Be able to appreciate the need for continuous improvement of products using

six sigma concepts [i] Be able to appreciate the role of six sigma practices in a global competitive

environment [j] Be able to apply modern probabilistic engineering skills [k]



AEEM 313 Modeling & Simulation of Physical Systems Date Prepared: February 2, 2004

Catalog data: 20-AEEM-313. Modeling & Simulation of Physical Systems. 3 cr. Modeling of physical systems, actuators, and sensors. Transient response, design of physical systems to meet constraints. Introduction to computer simulation and virtual laboratory.

Prerequisites: 20-ENFD-111 Computer Language; 20-ENFD-102 Mechanics II; 15-MATH-273 Differential Equations; 15-PHYS-203 Physics III

Textbook: Modeling and Simulation of Dynamic Systems, R.L. Woods and K.L. Lawrence, Prentice-Hall, 1997

References: None.Coordinator: Bruce K. Walker, Associate Professor of Aerospace Engineering & Engineering

Mechanics, 745B Baldwin, 556-3552, [email protected] Objectives: The student will be able to

1. Set up the differential equations governing a physical system [a, e]2. Model a given system using state space methods [a, e]3. Simulate the response of a system using SimuLINK [b, j, k]4. Model and simulate a linear mechanical system [a, b, e]5. Model and simulate an electrical system based on Kirchoff’s Laws [a, b, e]6. Model and simulate a fluid system (viscosity, Reynolds number effects,

capacitance) [a, b, e]7. Model and simulate a thermal system (convection, conduction, and radiation)

[a, b, e]8. Linearize a non-linear system model about a nominal condition [a]9. Experience participation in a team design effort [d]10. Present results in a technical report [c, g]

Topics Covered: Introduction to modeling and simulation; differential equation models; state space methods; Laplace transforms and the frequency domain (transfer function) approach; introduction to SimuLINK; modeling of mechanical systems; modeling of electrical systems; modeling of fluid systems; modeling of thermal systems; report preparation and presentation of results.

Computer usage: SimuLINKProfessional Experience:

Mathematics; Engineering; Design Experience


1, 2, 3, 4 and 6


Ability to apply mathematics, science, and engineering principles [a] Ability to design and conduct numerical experiments and analyze data [b] Ability to analyze and design a system [c] Ability to formulate engineering problems [e] Ability to write technical reports [g] Ability to use modern engineering tools and skills (SimuLINK) [j, k] Ability to work on a team design effort [d]



AEEM 329 Fundamentals of Engineering Measurements Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-329. Fundamentals of Engineering Measurements. 3 cr. Principles of modern computer-based engineering measurements, sensors, data acquisition systems, signal processing, data storage and display.

Prerequisites: 15-PHYS-201 - 203 Physics I, II, & III; 15-PHYS-211 - 213 Physics Laboratory I, II, & III

Textbook: Measurement and Instrumentation Principles, Alan S. Morris, Butterworth, 2001References: B. Paton, Fundamentals of Digital Electronics, Nat. Instr. Corp., 1998; LabView

Graphical Programming for Instrumentation, Nat. Instr. Corp., 1998; The Measurement, Instrumentations, and Sensors Handbook, CRC Press, 1999; class notes at http://www.ase.uc.edu/~pnagy/.

Coordinator: Peter Nagy, Professor of Aerospace Engineering & Engineering Mechanics, 731 Rhodes, 556-3353, [email protected]

Course Objectives: The student will be able to

1. analyze and design simple digital networks for measurement control, data acquisition, and data evaluation purposes. [a, b, k]

2. understand the basic operation of analog sensors and signal conditioning methods. [a, k]

3. operate different types of virtual instrumentation such as digital oscilloscopes, signal analyzers, data loggers, function generators, multimeters, and general purpose input/output devices. [b, k]

4. design and build simple virtual instruments in LabView for measurement control, data acquisition, and data evaluation purposes. [b, c, e, k]

5. design simple experiments to measure fundamental engineering quantities and to interface different types of sensors to computers through either analog-to-digital converters or serial/parallel interfaces. [b, c, e, k]

6. compare analytical predictions and experimental results and analyze their differences. [b]

7. present the results of laboratory measurements in formal laboratory reports. [g]Topics Covered: Basic concepts of engineering measurements, fundamentals of digital electronics,

computer-based instrumentation, data acquisition, computer-based signal processing, data evaluation, correlation estimation, error assessment, sensors,; active and passive transducers, examples of engineering measurements, displacement, velocity, acceleration measurements, force, weight, torque, time, frequency, phase, temperature.

Computer usage: LabViewProf. Experience: Engineering; General Education; Design ExperienceAEEM Program Objectives:

2, 3, 4, and 6


Combine mathematical, scientific, and engineering principles [a]. Design and conduct experiments [b, c] Identify, formulate and solve engineering problems [e]. Communicate through technical discussions and written reports [g]. Use modern engineering techniques, skills, and tools [k].

AEEM 342 Fundamentals of Aerodynamics Date Prepared: February 2, 2004

Catalog data: 20-AEEM-342. Fundamentals of Aerodynamics. 3 cr. Principles of ideal fluids and aerodynamics: potential theory, flow of perfect fluids about 2-D bodies. Lift and pitching moment of an airfoil of infinite span. Panel method.

Prerequisites: 15-MATH-252 - 254 and 256 – 258 Calculus II, III, & IV; 15-PHYS-201 Physics I; 20-ENFD-383 Basic Fluid Mechanics.


http://www.ase.uc.edu/~pnagy/


Textbook: Fundamentals of Aerodynamics, 2nd edition, J.D. Anderson, McGraw-Hill, 1991 References: Foundation of Aerodynamics, Bases of Aerodynamic Design, 4th edition, Arnold

M. Kuethe and Chuen-Yen Chow, John Wiley & Sons, 1986Coordinator: Ephraim Gutmark, Professor of Aerospace Engineering & Engineering

Mechanics, Ohio Eminent Scholar, 799 Rhodes, 556-1227, [email protected]


1. Understand basic concepts of fluid mechanics including: conservation equations, stream function, vorticity, strain, circulation, rotational flow, potential flow [a, e]

2. Apply Bernoulli’s equation to solve aerodynamic problems [a, e]3. Use the superposition principle to solve potential flow problems [a, e]4. Understand physics of lift generation [a, j]5. Apply existing panel methods to calculate flow & forces on nonlifting &

lifting bodies [k]6. Project: design an airfoil for desired specifications. [c, g]

Topics Covered: Basic laws & concepts of fluid mechanics, aerodynamics & thermodynamics: shear stress, viscosity, ideal & real fluids, aerodynamic forces & moments, control volume.

Review of vector algebra and integrals, & application in fluid dynamics. Stokes, divergence, & gradient theorems.

Conservation equations: mass, momentum, energy. Integral & differential formulation.

Pathlines and streamlines. Substantial derivative. Angular velocity, vorticity, strain, circulation. Potential & rotational flows.

Stream & potential functions. Bernoulli’s equation and applications in incompressible flows. Superposition of elementary potential flows. Flows over bodies, cylinders,

generation of lift. Kutta-Joukowski Theorem. General panel method solution for non-lifting bodies Lifting airfoils and circulation, thin airfoil theory. Kutta conditions. Vortex panel method for general lifting airfoils, symmetric and cambered.

Comparison between theory and experiments. Stall.Computer usage:Professional Experience:



1, 2, and 4




Be able to apply mathematical, scientific, & engineering tools to homework, exams, & projects [a]

Identify, formulate, & solve engrg problems in homework, exams, & projects [e]

Be able to discuss contemporary issues e.g. high lift devices, micro-aircraft, high speed flight, maneuverability, etc. [j]

Be able to apply modern engineering skills through homework & projects requiring the use of a computer to calculate an airfoil flow field [use of a panel code] & to graphically analyze the results [k]

Be able to design an airfoil for maximum lift & desired pitch movement [c]



AEEM 352 Vibration Analysis Date Prepared: February 2, 2004

Catalog data: 20-AEEM-352. Vibration Analysis. 3 cr. Free and forced vibrations of systems with one and many degrees of freedom; introduction to continuous systems; computational techniques.

Prerequisites: 20-ENFD-103 Mechanics III; 20-MATH-273 Diff Equations; 20-MATH-276 Matrix Methods or equivalent

Textbook: Engineering Vibrations, 2nd ed., D. J. Inman, Prentice-HallReferences: None.Coordinator: James Wade, Associate Professor of Aerospace Engineering & Engineering


1. Set up the equations of motion for discrete parameter vibration systems. [a]2. Identify spring and damping components for simple systems and use to

determine the natural frequency of vibration and damping ratio. [a, e]3. Use the energy method to determine the natural frequency of 1 dof systems. [a]4. Calculate the initial condition response of 1 dof systems. Use complex

variable representation of response and relate to real response. [a]5. Solve the eqn of motion for 1 dof with damping & determine the different

solutions associated with underdamped, critically damped & overdamped response [a]

6. Determine the frequency response of simple 1 & 2 dof systems under various forms of harmonic excitation. Identify and compute the resonance condition, beat phenomena, and vibration isolation. [a, e]

7. Set up the required convolution integrals and appropriate numerical solution methods, to compute the response of a system to arbitrary excitation. [a]

8. Use Fourier series to represent any periodic function as an infinite sum of harmonic functions. Apply to calculation of response of a vibration system to arbitrary periodic input. [a]

9. Use eigenvalue and eigenvector methods of matrix algebra to compute natural frequencies and mode shapes for multi degree of freedom systems. [a, e, k]

10. Obtain the decoupled modal equations using orthogonality of modes. [a, k]11. Derive the partial differential eqns of motion for some simple continuous

system models (string, beam, etc.). Determine natural frequencies and mode shapes as the eigenvalues & eigenfunctions of the associated Sturm-Liouville problem. [a, k]

Topics Covered: Harmonic motion, viscous damping, modeling and energy methods, stiffness, design considerations, stability, harmonic excitation of damped and undamped systems, base excitation and rotating unbalance, impulse response function and response to an arbitrary input, response to an arbitrary periodic input, multi DOF systems (damped and undamped), eigenvalues and natural frequencies, modal analysis (forced and unforced response), Lagrange’s equations, vibrations of strings, cables, rods and bars, bending vibrations of beams.


Mathematics; Engineering; General Education




2 and 3


Apply mathematical, scientific, & engineering tools from homework and examinations [a]

Identify, formulate, & solve engineering problems in homework & examinations [e]

Apply modern engineering skills through homework & projects requiring the use of a computer [k]



AEEM 360 Numerical Methods for Engineering Design Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-360. Numerical Methods for Engineering Design. 3 cr. Interpolation and approximation, numerical integration, solutions of equations, systems of equations. Solution of ordinary differential equations; computer design problems with application to Aerospace Engineering and Engineering Mechanics.

Prerequisites: 15-MATH-251 - 254 (Calculus I through IV); 15-MATH-273 Differential Equations; 15-MATH-276 Matrix Methods; 20-ENFD-101, 102, 103 (Mechanics I, II, III)

Textbook: Applied Numerical Analysis Using Matlab, L. V. FausettReferences: Numerical Methods, R. Hornbeck, Quantum Press, 1975

Applied Numerical Methods, B. Carnahan, H. Luther, and J. Wilkes, Wiley, 1969.Coordinator: Prem Khosla, Professor of Aerospace Engineering & Engineering Mechanics, 745C

Baldwin, 556-3551, [email protected] Objectives: The student will be able to

1. Write a Lagrangian interpolation program for 1 & 2 dimensional data in MATLAB [a, k]

2. Write a MATLAB program for numerical integration using Trapezoidal Rule, Simpson’s Rule, and Gauss Quadrature. [a, k]

3. Write a MATLAB program for fixed point, secant, and Newton’s Method for finding roots/zeros of functions. [a, k]

4. Solve simultaneous sets of linear algebraic equations using direct and iterative methods (Gauss elimination, Jacobi, SOR) using MATLAB [a, k]

5. Solve simultaneous sets of non-linear equations using Newton’s Method [a, k]6. Compute finite difference representation of 1st, 2nd, 3rd, and 4th derivatives of given

accuracy, using Taylor series. [a, k]7. Distinguish between a boundary value and an initial value problem and choose

appropriate methods of solution [a]8. Write a MATLAB program solving a two-point boundary value problem [a, c, k]9. Write a MATLAB program integrating several ordinary 1st order diff. equations [a,

k]10. Appreciate the concepts of order of accuracy, errors, & stability & their role in

advanced applications [i, j]11. Apply numerical methods to solve engineering problems:

2-D Lagrangian interpolation of data [b] Application of Newton’s method to Prandtl-Meyer function [a, e] Parametric analysis of length of a heat exchanger piping system [a, e] Design of beam with displacement and stress constraints [b, c, e] Maneuvering of an astronaut in outer space [b, c, e]

12. Present results in the form of a technical report [g]Topics Covered: MATLAB, Lagrangian interpolation, numerical integration, Newton’s method, finite-

differences, and numerical solution of differential equations. Students perform application of numerical techniques for the analysis and design of engineering problems of interest to aerospace engineers.

Computer usage: MATLABProfessional Experience:

Mathematics; Engineering; General Education, Design Experience


2, 3, 4, and 6




Apply computational tools to solve engineering problems from homework and projects [a, k]

Convert mathematical descriptions of a problem into numerical for digital implementation [e, k]

Apply computational techniques for open-ended problems and analyze numerical data [b, c]

Written and oral communications skills through class projects and discussions [g] Employ state of the art computer tools and understand need to adapt; learn more for

advanced sophisticated practical problems [i, k] Knowledge of techniques required for the solution of problems and an appreciation

of importance of computers as a vital tool in industry [j]



AEEM 361 Integrated Aircraft Engineering Date Prepared: February 2, 2004

Catalog data: 20-AEEM-361. Integrated Aircraft Engineering. 3 cr. Students will learn aircraft, spacecraft, & propulsion system nomenclature. Students will develop an appreciation for aerospace vehicles & propulsion systems through case studies of or in response to previous preliminary design efforts, or via case studies from AIAA or aerospace contractors. Students will work in small groups on several aspects of a component or subsystem design of an aerospace vehicle or propulsion system component.

Prerequisites: 15-MATH-251 - 254 (Calculus I through IV); 15-MATH-273 Differential Equations; 20-ENFD-101, 102, 103 (Mechanics I, II, III)

Textbook: Notes from instructorReferences: Engineering Vibrations, 2nd ed., D.J. Inman, Prentice Hall

Aircraft Structures for Engineering Students, 3rd ed., T.H.G. Megson, WileyCoordinator: James Wade, Associate Professor of Aerospace Engineering & Engineering


1. Identify the flight envelope, with gust effects, and its relation to the design of an aerospace vehicle [a, j]

2. Relate the wing loading, due to various maneuvers, of the flight vehicle to the design points on the flight envelope and design structural elements [a, e]

3. Apply the flight loads and analyze open and closed sections for shear flow and boom stresses or loads (both continuous and area skin) [a, e]

4. Use energy methods to find loads & stresses in frames and bulkheads; use instructor-developed force-displacement equation for a 4 dof beam element, from applying Lagrange’s equation, to determine the first bending frequency of a wing [a, c, d, i]

5. Use a given wing layout, subjected to a wing loading, and design the wing with stringers and ribs for a specific point on the flight envelope as a group project [a, c, d]

6. Approximate the wing mass distribution & boundary conditions, & estimate the first bending frequency [a, h, k]

7. Explain & present problem solution as a team effort report and a report on previous AIAA case studies [b, c, d, f, g]

Topics Covered: The application of Castigliano’s first theorem to statically indeterminate structures, column buckling as applied to the design of rib spacing, loads on structural components, bending of open and closed sections, shear of open section beams, shear of closed section beams, torsion of closed and open section beams, structural idealization and its effect on the analysis of open and closed sections; semi-monocoque structures, tapered beams, fuselage frames & wing ribs, factors of safety: flight envelope, load factor determination, symmetric maneuver loads.




1, 2, 3, 4, 5 and 6


An ability to apply knowledge of mathematics, science, and engineering principles to problem solving [a]

An ability to analyze and interpret data [b] An ability to design a wing rib stringer configuration based on specified

loading [c]



An ability to function in a team environment & communicate effectively [d, g]

An ability to identify and solve engineering problems [e] An awareness of professional and ethical responsibility [f] A knowledge of contemporary issues [j] A recognition of the need to learn present-day advanced tools [i] An ability to certify the validity of computations for flying quality [h] An ability to use computational tools to obtain numerical results [k]



AEEM 382 Aerospace Vehicle Performance Date Prepared: February 2, 2004

Catalog data: 20-AEEM-382. Aerospace Vehicle Performance 3 cr. Development of equations for vehicle motion. Performance of aircraft and rockets in the atmosphere and in space.

Prerequisites: 20-ENFD-102 Mechanics II; 15-MATH-273 Differential Equations; 20-AEEM-342 Fundamentals of Aerodynamics

Textbook: Fundamentals of Flight, 2nd ed., R.S. Shevell, Prentice Hall: 1989Space Mission Analysis & Design, 3rd ed., J.R. Wertz and W. Larson, Microcosm Press: 1999

References: NoneCoordinator: James Wade, Associate Professor of Aerospace Engineering & Engineering


1. Compute orbit trajectories and compute velocity requirements to reach specific orbits [a, e]

2. Determine V for a rocket, and determine rocket performance requirements to reach a specific orbit, including possible rocket staging [a, e]

3. Estimate lift and drag characteristics for subsonic aircraft [a]4. Formulate and solve quasi-steady performance problems using simple

analytical models [a]5. Use the computer to generate algorithms and code to solve more complex

performance problems using numerical models [k]6. Do preliminary wing and propulsion system sizing of a vehicle to meet

specific mission requirements [c, j]7. Communicate solutions of engineering problems in written and oral

presentations [g]Topics Covered: Equations of motion for vehicles in and outside the atmosphere. Elementary

astronautics. Solution of rocket equations. Preliminary design of space missions. Review of wing aerodynamics. Elementary airbreathing propulsion system performance. Performance calculation for air vehicles and preliminary sizing to meet mission specifications.

Computer usage: MATLABProfessional Experience:



1, 2, 3, and 6


Ability to apply math and engineering principles to solve orbit and aircraft performance problems [a, e]

Ability to do preliminary design of an aircraft configuration to meet realistic performance specifications [c, j, k]

Ability to communicate in written and oral presentations [g] Ability to use computer codes (MATLAB) to solve problems [k]



AEEM 403 Fundamentals of Control Theory Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-403. Fundamentals of Control Theory 3 cr. Fundamentals of feedback control system modeling, transfer functions, root locus and frequency response methods.

Prerequisites: 15-MATH-273 Differential Equations; 20-AEEM-313 Modeling & Simulation of Physical Systems

Textbook: Feedback Control Systems, 4th ed., C.L. Phillips & R.D. Harbor, Prentice Hall, 2000

References: NoneCoordinator: Bruce Walker, Associate Professor of Aerospace Engineering & Engineering

Mechanics, 745B Baldwin, 556-3552, [email protected] Objectives: The student will be able to

1. Construct dynamic models (circuits, mechanical motion, etc.) of systems and determine transfer functions [a]

2. Draw block diagrams and/or signal flow graphs of physical systems [a, e]3. Relate transient time response characteristics to Laplace transform poles and

zeros [a]4. Evaluate closed loop control system characteristics (stability, sensitivity,

steady state error, etc.) [a]5. Design and analyze performance of control systems using the root locus

method [a, c, k]6. Use frequency response methods to analyze stability and to design a control

system to meet closed loop specifications using PID and lead/lag compensation [e, k]

Topics Covered: Review of dynamic models, Laplace transforms and transfer functions. Block diagrams and signal flow graphs and their reduction. Open loop and closed loop transfer functions. Time response specifications and stability and their relationship to pole and zero locations. Sensitivity and steady state error. Root locus analysis and design. Basics of frequency response and Bode plots. Compensator design using frequency response methods.



AEEM Program Objectives:ABET Criteria Addressed:

Ability to construct dynamic models and models of feedback systems [a] Ability to relate pole-zero configuration to transient and steady state

response [a, e] Ability to design a control system to meet performance specs using

appropriate computer tools [a, c, k]



AEEM 430 Matrix Structural Analysis Date Prepared: February 2, 2004

Catalog data: 20-AEEM-430. Matrix Structural Analysis 3 cr. Computer oriented methods for solving determinate and indeterminate structures with emphasis on trusses, frames, and beams; extensive static analysis using the force-displacement method; dynamic response of bar and beam elements using lumped and consistent mass matrices.

Prerequisites: 20-ENFD-375 Basic Strength of Materials or equivalent; 20-AEEM-352 Vibration Analysis.

Textbook: Matrix Structural Analysis, W. McGuire, H.H. Gallagher& R.D. Zieman, 2nd ed., Wiley & Sons.

References: NoneCoordinator: Ala Tabiei, Associate Professor of Aerospace Engineering & Engineering Mechanics,

722 Rhodes, 556-3367, [email protected] Objectives: The student will be able to

1. Develop the Force Displacement Equation: 1) for the axial force member (locally & globally); 2) for the frame (beam) element (locally & globally); 3) use these elements in the set up of multi-degree of freedom structural configurations; 4) apply boundary conditions, invert the reduced stiffness matrix, and obtain the nodal replacements; 5) calculate axial loads, shear forces, and bending moments [a, b]

2. Use the direct stiffness method and develop the global force displacement equations for structural trusses that have been synthesized from bar elements. [a, b, h, k]

3. Apply boundary conditions to the global force-displacement equation, partition, reduce, and condense the stiffness matrix in obtaining the nodal displacements, then using these displacements to find the element (bar) forces. [a, e]

4. Know the role of work and energy in the development of the stiffness matrix, and the importance of Maxwell’s reciprocal theorem for linearly elastic structures. [a]

5. Use the equilibrium matrix to develop the complete stiffness matrix from a given flexibility matrix. [a]

6. Calculate the entries, using equilibrium methods, for the 12 dof frame element for the local coordinate system, transform the element to a global coordinate system, and use the element in the structural analysis of a built-up frame structure. [a, b, e, h, j, k]

7. Resolve the given loads on a frame element into the appropriate loads at the nodal points. [a]

8. Dynamic response of bar and beam elements using lumped and consistent mass matrices [a, k]

Topics Covered:

Degree of freedom; detailed development of the stiffness matrix for the axial force member and the frame element; equilibrium of internal forces with external nodal forces in the development of the algebraic equations for the Direct Stiffness Method; inversion of the reduced stiffness matrix to obtain the flexibility matrix, determinate and indeterminate structures, and work and energy; Maxwell’s reciprocal theorem for Hookean structures; reconstruction of the complete stiffness matrix from the flexibility matrix and the equilibrium matrix; 12 dof beam element; reduction of distributed and contracted and concentrated loads to nodal point loads.






1, 2, 4, 5, and 6


Ability to integrate the knowledge of theory with mathematical and engineering analysis [a]

Ability to analyze the numerical results for possible errors and engineering accuracy [b]

Ability to formulate the problems in the form of stiffness matrices [e] Emphasis on computer solutions for large assembled systems [h] Ability to use modern computational tools [k] Ability to identify contemporary issues and practices in engineering problem

solving [j]



AEEM 438 Mechanics of Solids Laboratory Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-438. Mechanics of Solids Laboratory 3 cr. Experimental stress analysis. Strain gauge rosettes. Static and dynamic measurements. Stability

Prerequisites: 20-ENFD-375 Basic Strength of Materials; 20-AEEM-329 Engineering Measurements

Textbook: F. P. Beer & E. R. Johnston, Jr., Mechanics of Materials, 2nd ed., McGraw-Hill, 1992.

References: “MIL-HDBK-5, Metallic Materials & Elements for Flight Vehicle Structures,” U. S. Government, 1966; class notes at http://www.ase.uc.edu/~pnagy/

Coordinator: Peter Nagy, Professor of Aerospace Engineering & Engineering Mechanics, 731 Rhodes, 556-3353 [email protected]


8. Analyze the state of deformation of simple structures under combined loading conditions and design appropriate strain gauge rosettes for their experimental investigation [a, b]

9. Use computer-based instrumentation to analyze structural deformations under different loading conditions [b, k]

10. Use digital signal processing techniques to reduce experimental uncertainties and to evaluate the measured data [b, e]

11. Analyze and evaluate the repeatability, reproducibility, and accuracy of structural measurements [b]

12. Understand material behavior under elastic & plastic loading conditions [a]13. Understand reciprocity concepts and their application in structural

measurements [a]14. Compare analytical predictions and experimental results and analyze their

differences [b, k]15. Present the results of laboratory measurements in formal laboratory reports [g]

Topics Covered: Computer-based instrumentation, strain gauge rosettes and bridges, strain transformation, tensile machine, displacement and strain measurements in beams and plates, torque transducers, moment transducers, combined stress and strain, dynamic deformations, Maxwell's Reciprocity Theorem, uniaxial tension, plastic yield, beam columns, buckling.


Engineering; General Education


2, 3, 4, and 6


An ability to combine mathematical, scientific, and engineering principles [a] An ability to design and conduct experiments [b] An ability to identify, formulate and solve engineering problems [e] An ability to communicate through technical discussions and written reports [g] An ability to use modern engineering techniques, skills, and tools [k]



AEEM 445 Gas Dynamics Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-445. Gas Dynamics 4 cr. Equations of one and two-dimensional gas motion. Speed of sound, normal and oblique shock waves, expansion wave theory. Applications are presented for diffusers and nozzles, wind tunnel design, jet exhausts, and airfoils.

Prerequisites: 15-MATH-254 Calculus IV, 15-MATH-276 Differential Equations, 20-ENFD-382 Basic Thermodynamics, 15-ENFD-383 Basic Fluid Mechanics; 20-AEEM-342 Fundamentals of Aerodynamics

Textbook: Fundamentals of Aerodynamics, 2nd ed., John D. Anderson: McGraw-Hill, 1991Introduction to Fluid Mechanics, 5th ed., Fox and MacDonald: Wiley & Sons, 1998.

References: Gas Dynamics, 2nd ed., James E. A. John, Allyn & Bacon Publishers, 1984Coordinator: Karman Ghia, Professor of Aerospace Engineering & Engineering Mechanics,

681 Rhodes, 556-3243 [email protected] Objectives: The student will be able to

8. Understand the concept of Conservation Equations in integral form for a Control Volume [a]

9. Develop proficiency in manipulating the isentropic flow relations for a perfect gas Determine the expression for the speed of sound for a perfect gas [a]

10. Explain the concepts of zone of silence and zone of action for supersonic flows [a]

11. Determine the flow properties inside a converging-diverging nozzle for [e]isentropic conditions; flows with normal shock; flows with oblique shocks and Prandtl-Meyer waves

12. Design a high speed wind tunnel, taking into account factors such as compressor pumping time, model size and balance, and present results as a technical report [b, c, f, g, h, i, j, k]

13. Compute lift and drag using shock expansion theory for airfoils [a, e, k]14. Compute the flow-field variables in jets exhausting in quiescent air [a, e, k]15. Sketch the Fanno and Raleigh line T-S diagrams and compute the associated

flow variables [e]Topics Covered: Basic equations of mass, momentum, and energy from control volume concepts;

Wave propagation and the speed of sound; One-dimensional isentropic flow and/or normal shock waves; Application to converging-diverging nozzles and diffusers, and wind tunnels; Oblique shock waves and Prandtl-Meyer flow in nozzles and diffusers; Application to under and over expanded jets and airfoils; Friction and heat addition for subsonic flows in constant area ducts; Design of supersonic inlet or nozzle using shock-expansion theory; Design of supersonic nozzle in presence of friction and heat addition.

Computer usage: Design of supersonic inlet or nozzle using shock-expansion theory; design of supersonic nozzle in presence of friction and heat addition.

Professional Experience:



1, 2, 3, 4, and 6


Know how to apply mathematical, scientific, and engineering analyses tools appropriate to gas dynamics [a]

Be able to identify, formulate, and solve engineering problems related to gas dynamics in homework, project, and examinations [e]

Calculate lift and drag on supersonic airfoils, determine flow fields in the



wake of under and over expanded nozzles, etc. [a, e, k] Utilize modern engineering skills in the homework and project requiring the

use of computer software in the detailed computation of an optimum nozzle configuration, wind-tunnel design, etc. [b, c, f, g, h, i, j, k]



AEEM 452 Flight Mechanics Date Prepared: February 2, 2004

Catalog data: 20-AEEM-452. Flight Mechanics 3 cr. Equations of motion of aircraft. Longitudinal and lateral dynamics. Automatic control of aircraft

Prerequisites: 15-MATH-273 Differential Equations, 20-ENFD-103 Mechanics III; 20-AEEM-313 Modeling and Simulation of Physical Systems

Textbook: Flight Stability and Automatic Control, 2nd ed., R. Nelson, McGraw-Hill, 1998

References: None.Coordinator: Gary Slater, Professor of Aerospace Engineering & Engineering Mechanics,


1. Identify the Euler angle set used to describe the rotational motion of a rigid aircraft or spacecraft. [a]

2. Derive and linearize the aircraft equations of motion for arbitrary reference flight conditions. [a]

3. Determine appropriate linear stability derivatives for aircraft motion using reference material and basic aerodynamic theory, in dimensional and non-dimensional form. [a, e, j]

4. Identify the difference in “stick-fixed” and “stick-free” stability properties of aircraft and estimate hinge moments and stick forces. [e]

5. Solve numerically for the modes of motion, and identify the modes of motion from the mode shapes and eigenvectors of the linearized dynamics model. [a, k]

6. Utilize reduced order models to compute approximate modes of motion. [a, k]

7. Design control surfaces and size the horizontal and vertical tails to give required stability and control characteristics and relate these characteristics to the “handling qualities” of aircraft. [c, e]

8. Apply simple feedback theory to demonstrate how a stability augmentation system works. [a]

Topics Covered: Flight mechanics terminology and reference systems. Six degree of freedom equations of motion for rigid vehicles operating in the atmosphere or in space. Linearization of equations about a reference condition, and analysis of motion. Determination of dimensionless and dimensional aerodynamic derivatives and relationship to aircraft geometry. Application of stability and control design criteria to meet aircraft handling qualities criteria.

Computer usage:Prof. Experience: Mathematics; Engineering; Design ExperienceAEEM Program Objectives:

1 and 2


Ability to derive and linearize aircraft equations of motion [a] Ability to estimate stability derivatives from basic theory and reference

data [a, e, j] Ability to compute linearized modes and mode shapes [a, k] Ability to design stability and control surfaces to meet required “handling

qualities” [c]AEEM 456 Applied Aerodynamics Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-456. Applied Aerodynamics 3 cr. Theory and application of a vortex lattice code, introduction to the concept of a viscous flow, presentation of the Navier Stokes and boundary layer equations, theory and application of 2D



boundary layer code, introduction to turbulence modeling and application for boundary layers

Prerequisites: 20-ENFD-383 Basic Fluid Mech.; 20-AEEM-342 Fnd of Aerodyn.; 20-AEEM-445 Gas Dyn.; 20-AEEM-360 Num. Meth. Eng. Des.

Textbook: Fundamentals of Aerodynamics, 2nd ed., John D. Anderson, McGraw-Hill: 1991References: Fluid Dynamic Drag: Practical Information on Aerodynamic Drag and

Hydrodynamic Resistance, Sighard F. Hoerner, Hoerner Fluid Dynamics, 1965 (ISBN 9991194444)XFOIL 6.9 User Guide, Mark Drela and Harold Youngren, PDF file available at http://raphael.mit.edu/xfoil/Foundations of Aerodynamics: Bases of Aerodynamic Design, 4th ed., Arnold M. Kuethe and Chuen-Yen Chow, John Wiley & Sons: 1986 (ISBN 0471806943)

Coordinator: Paul Orkwis, Associate Professor of Aerospace Engineering & Engineering Mechanics, 478 ERC, 556-3366 [email protected]


1. Calculate the lift, drag, and moment on any given 2D airfoil including boundary layer effects using X-Foil [a, c, d, e, g, i, j, k]

2. Know the nomenclature for the NACA airfoil series [a]3. Be able to understand the basic concepts of finite wing theory: downwash;

induced drag; elliptical lift distribution; classic lifting line theory [a]4. Assess the performance characteristics of a wing using Prandtl’s lifting line

and a given vortex lattice code [a, b, d, e, g, k]5. Estimate the drag on any given 3D wing including end effects [a, e, k]6. Apply the concept of Area Ruling over all flow regimes [a]7. Apply boundary layer concepts & understand when appropriate to apply [a]8. Define important aerodynamic quantities such as Reynolds number, Mach

number, boundary layer thickness, angle of attack, sweep, dihedral, downwash, & aspect ratio [a]

Topics Covered: Navier-Stokes and boundary layer equations, integral boundary layer methods, Reynolds number, Mach number, boundary layer thickness, angle of attack, sweep, dihedral, downwash, and aspect ratio

Application of XFOIL (a coupled panel and integral boundary layer method) to get an appreciation for NACA series airfoil definitions, boundary layer concepts, integral boundary layer methods, effects of Reynolds number and laminar, transitional, and turbulent flow

Finite wing theory, downwash and induced drag, classic lifting line theory and elliptical lift distribution

Computer usage: X-FoilProfessional Experience:



1, 2, 3, 4, and 6


Ability to apply knowledge of modern aerodynamic analysis [a, e, j, k] Ability to interpret lift and drag data [b, e, j, k] Ability to design an airfoil [c, e, i, j, k] Ability to present results in technical reports [g] Ability to work in a team environment [d]


http://raphael.mit.edu/xfoil/


AEEM 462 Integrated Spacecraft Engineering Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-462. Integrated Spacecraft Engineering 3 cr. Application of fundamentals earned in previous courses to the design and construction of a simple device or system, to meet specified design objectives. Formal documentation/presentation of results. One class hour/wk for introduction, discussion of approaches, problems and progress reports. Two hours/wk design and/or fabrication in lab. Students spend time normally devoted to homework with design and construction. The formation of the groups and definition of projects will consider the senior options students wish to take.

Prerequisites: 15-MATH-251 - 254 (Calculus I through IV); 15-MATH-273 Differential Equations; 20-ENFD-101, 102, 103 (Mechanics I, II, III), 20-AEEM-111 Intro to Spacecraft Eng

Textbook: Space Mission Analysis and Design, J.R. Wertz and W.J. Larson, 3rd edition, Microcosm/Kluwer, 1999

References: None.Coordinator: Trevor Williams, Professor of Aerospace Engineering & Engineering Mechanics,


1. Determine suitable orbits and required maneuvers, & simulate the resulting groundtracks [a, k]

2. Identify a suitable launch vehicle, & calculate the on-orbit propellant required for the mission [a, e]

3. Determine mass and power budgets for the spacecraft for the specified mission [c, j]

4. Produce a physical layout of the spacecraft [c, e]5. Perform a preliminary design of an attitude control system (active, passive, or

semi-active) [c, k] 6. Design a power system, sizing both solar arrays & batteries for the given

mission [c,e,k]7. Use link budget analysis to design a spacecraft uplink and downlink

communication system [e, j]8. Perform a preliminary spacecraft thermal analysis & design a suitable thermal

control system [a, e, k]9. Perform a preliminary spacecraft cost analysis [h, j]10. Experience participation in a design team effort [d]11. Make a professional presentation as a team to a panel of faculty members [g]

Topics Covered: Discussions of the design process and constraints and design tradeoffs; orbital maneuvers analysis; launch vehicle options; mass and power budget analysis; effects of the space environment on the spacecraft; attitude control hardware options; propulsion systems; energy budgets for batteries; communication system: data rates and link budgets; thermal analysis: effects of external properties vs. active thermal control; parametric cost analysis; intermediate report preparation and presentation of results.

Computer usage: Satellite ToolKitProfessional Experience:





1, 2, 3, 4, 5 and 6


Know how to apply engineering, science and mathematical tools [a] Demonstrate the ability to design a spacecraft and its components and estimate

its cost [c, e] Be able to work on assigned projects in teams [d] Be able to communicate results of projects in both oral and written reports [g] Be able to use existing orbital analysis packages and write computer programs

to accomplish project objectives [k] Be able to perform a preliminary spacecraft cost analysis [h, j]



AEEM 474 Airbreathing Propulsion Date Prepared: February 2, 2004

Catalog data: 20-AEEM-474. Airbreathing Propulsion 3 cr. Aero-thermodynamic data: foundations of propulsion theory. Cycle thermodynamics. Turbomachinery. Aerodynamic design of compressors and turbines.

Prerequisites: 20-ENFD-382 Basic Thermodynamics; 20-ENFD-383 Basic Fluid Dynamics; 20-ENFD-385 Basic Heat Transfer; 20-AEEM-445 Gas Dynamics

Textbook: Gas Turbine Theory, H. Cohen, G.F.C. Rogers and H.I.H. Saravanamuttoo, Longman 2e

References: Elements of Gas Turbine Propulsion, J. Mattingly, McGraw-Hill.Coordinator: Shaaban Abdallah, Professor of Aerospace Engineering & Engineering

Mechanics, 721 Rhodes, 556-3321 [email protected] Objectives: The student will be able to

1. Define the principal definitions, concepts, cycles, and basic physical laws. [a, e, h]2. Draw and label ideal and real, and carry out performance analysis for, air-breathing

propulsion systems: [a, e, j]a. turbojetb. turbojet with afterburnerc. turbofan engined. turboprop enginee. turboshaft engine

3. Apply the energy principles in engine components: [a, e, j]a. axial and centrifugal compressorsb. axial and radial gas turbines

4. Carry out component and engine performance analysis [e, j]a. intake pressure recoveryb. nozzlesc. compressor and turbine efficienciesd. matching of components (compressor and turbine)

5. Sketch a gas turbine combustor and explain the flow condition in its various zones [a, j]

Topics Covered: Fundamental propulsion system performance, equations, Brayton cycles, analysis of airbreathing engines (turbojet, turbofan, turboprop, and turboshaft), component performance and efficiencies.


Engineering; Design Experience


1, 2, and 4


An ability to apply knowledge of thermodynamics, gas dynamics, and heat transfer to propulsion systems [a]

Ability to identify the significant engine performance parameters and their role in engine selection for various applications [e]

Recognize environmental constraints and their impact on engine selection [h, j]

AEEM 502 and 512 Aircraft Design I & II Date Prepared: February 2, 2004

Catalog data: 20-AEEM-502/512. Aircraft Design I & II 4 cr. ea; 8 cr. total. Integrated vehicle system performance, mission/constraints. Aircraft design, analysis, trade studies, and optimization.



Prerequisites: 20-AEEM-382 Aerospace Vehicle Performance; 20-AEEM-445 Gas Dynamics; 20-AEEM-456 Applied Aerodynamics; 20-AEEM-452 Flight Mechanics

Textbook: Aircraft Design: A Conceptual Approach, Third Edition, Daniel P. Raymer, AIAA, New York, New York, 1999.

References:Coordinator: Awatef Hamed, Professor of Aerospace Engineering & Engineering Mechanics,

745E Baldwin, 556-3553 [email protected] Objectives: The student will be able to

1. Design and analyze an aircraft from needs and requirements given in an RFP [b, c, e]2. Synthesize aircraft layout of all major components [e, j]3. Define global and interface quantities required for the component design teams [g]4. Design aero-surfaces and select airfoils, estimate aircraft’s lift, drag, moment

characteristics [e]5. Select and install propulsion system [e]6. Calculate loads, layout and analyze structures, calculate weight and balance data [a,

e, k]7. Conduct stability and control analysis [a, e, k]8. Analyze flight performance [a, e]9. Accomplish sizing and performance trades and optimization [c, e, k]10. Experience participation in a design team effort [d, g, i]11. Make a professional presentation as a team to a panel of engineers from industry [g,

h, i]12. Prepare a well-documented team report of the design methodology and trade-off

studies [d, g, h, i]Topics Covered: Discussion of the RFP and design process, constraints and tradeoffs, aero-surface design,

lift and drag estimates, aerodynamic loads, structural analysis, weight balance, flight performance, stability and controls analysis, sizing optimization and propulsion system selection.

Computer usage: CompuFoil™Prof. Experience Engineering; Design ExperienceAEEM Program Objectives:

1, 2, 3, 4, and 6


Know how to apply engineering, science and mathematical tools [a] Know how to interpret specifications and performance data [b] Demonstrate the ability to design an aircraft and its components (wing, tail, etc.) [c,

e] Be able to schedule various tasks involved in the design and trade-off studies among

the team members [d] Be able to write progress reports and final report in an appropriate format and be

able to make an oral presentation on the design [g] Be able to access resources outside the assigned text and interact with industry or

government laboratory experts [i, j] Be able to use existing software packages effectively and write computer programs

to accomplish the objectives [k]AEEM 515 and 517 Spacecraft Design I & II Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-515/517. Spacecraft Design I & II, 4 cr. ea, 8 cr. total. 515: Introduction to space mission analysis and the principles of spacecraft design, space mission lifecycle, mission constraints and objectives. Cost Estimation. 517: Concepts of space subsystem design. Formal design of a space mission and associated spacecraft. Report preparation and formal presentation.

Prerequisites: 20-AEEM-403 Fundamentals of Controls; 20-AEEM-462 Integrated Spacecraft Eng

Textbook: Space Mission Analysis and Design, J.R. Wertz and W.J. Larson, 3rd edition, Microcosm/Kluwer, 1999



References:Coordinator: Trevor Williams, Professor of Aerospace Engineering & Engineering Mechanics,

735 Rhodes, 556-3221 [email protected] Objectives:


1. Interpret the requirements given in a Request for Proposal (RFP) to determine suitable orbits and required maneuvers [a, h, j]

2. Determine mass and power budgets for the spacecraft for the specified mission [e]

3. Produce a physical layout of the spacecraft [e, h]4. Perform a detailed design of an attitude control system [c, e]5. Design a power system sizing both solar arrays & batteries for the given

mission [c, k]6. Use link budget analysis to design a spacecraft uplink and downlink

communication system [c, k]7. Perform a detailed spacecraft thermal analysis, and so design a suitable

thermal control system [c, k]8. Perform a parametric spacecraft cost analysis [e]9. Experience participation in a design team effort [d, g, i]10. Make a professional presentation as a team to a panel of faculty members [g,

h, j]11. Prepare a well-documented team report of the design methodology and trade-

off studies [d, g, h, i]12. Access outside resources to complete knowledge required for the design [i]

Topics Covered: Discussions of the RFP; design process & constraints & tradeoffs; orbital maneuvers analysis; mass & power budget analysis; effects of space environment on spacecraft; attitude control hardware options; propulsion systems; energy budgets for batteries; communication system: data rates, link budgets; thermal analysis; effects of external properties vs. active thermal control; parametric cost analysis; report preparation & presentation of results.




1, 2, 3, 4, and 6




Know how to apply engineering, science and mathematical tools [a] Know how to interpret specifications and performance data [b] Demonstrate the ability to design a spacecraft and its components [c, e] Be able to schedule various tasks involved in the design and trade-off studies

between the team members [d] Be able to write progress reports and final reports in an appropriate format

and be able to make an oral presentation on the design [g] Be able to access resources outside the assigned text and interact with

industry or government laboratory experts [i, j] Be able to use existing software packages effectively and write computer

programs to accomplish the objectives [k] Be able to develop cost-effective spacecraft designs that are useful to society

[h]



AEEM 519 and 523 Engine Design I & II Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-519/523. Engine Design I & II 4 cr. ea & 8 cr. total. 519: Integrated propulsion/vehicle system performance, mission/constraints. Trade off studies design and off design cycle analysis and optimization. 523: Engine flow path and sizing. Intake, turbomachinery, combustor and exhaust system design. Report preparation and formal presentation

Prerequisites: 20-AEEM-382 Aerospace Vehicle Performance; 20-AEEM-445 Gas Dynamics; 20-AEEM-474 Airbreathing Propulsion

Textbook: Aircraft Engine Design, J.D. Mattingley, W.H. Heiser, and D.H. Daley, AIAA, New York, New York, 1987

References:Coordinator: Awatef Hamed, Professor of Aerospace Engineering & Engineering Mechanics,

745E Baldwin, 556-3553 [email protected] Objectives: The student will be able to

1. Construct an aircraft constraint diagram from RFP requirements [a, b, c, e, k]

2. Calculate the fuel required for a given mission using engine performance estimates [a, b, e, k]

3. Use an engine code to select the best design point parameters [c, e, k]4. Use an engine code to calculate off-design performance [e, k]5. Select an engine design point for a given mission and size the engine [b, c,

e, h, j]6. Define global and interface quantities required for the component design

teams [c, d]7. Outline design methods for all engine components [a, b, c]8. Design engine components [c, k]9. Experience participation in a design team effort [d]10. Make a professional presentation as a team to a panel of engineers from

industry [g, h, i]11. Prepare a well-documented team report of the design methodology and

trade-off studies [d, g, h, i]Topics Covered: Discussion of the RFP and design process and constraints, constraint analysis,

and mission analysis; engine selection (on-design analysis, off-design analysis, design point selection, and sizing); engine component design, fan, compressor, and turbine flow paths and blading design; combustor, afterburner, inlet, and nozzle design; report and presentation of results.




1, 2, 3, 4, and 6




Know how to apply engineering, science and mathematical tools [a] Know how to interpret specifications and performance data [b] Demonstrate the ability to design a propulsion system and its components

[c, e] Be able to schedule various tasks involved in the design and trade-off

studies among the team members [d] Be able to write progress reports and final report in an appropriate format

and be able to make an oral presentation on the design [g] Be able to access resources outside the assigned text and interact with

industry or government laboratory experts [i, j] Be able to use existing software packages effectively and write computer

programs to accomplish the objectives [k] Be able to understand and comply with environmental constraints [h]



AEEM 574 Aerodynamic Measurement Laboratory Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-574. Aerodynamic Measurement Laboratory 3 cr. Analysis of data, measurement of pressure, velocity, volume flow rate, and drag. Drag and lift evaluations on a lifting airfoil and bluff body experimentation. Experiments.

Prerequisites: 20-AEEM-329 Engg Measurements; 20-AEEM-342 Fundamentals of Aerodynamics; 20-AEEM-456 Applied Aerodynamics

Textbook: Aerodynamic Measurement laboratory notesReferences: Experimental Methods for Engineers, 6th edition, J.P. Holman, McGraw-Hill;

1994; Foundations of Aerodynamics, A.M. Kuethe & C-Y. Chow, Wiley & Sons: 1986

Coordinator: Peter J. Disimile, Associate Professor of Aerospace Engineering & Engineering Mechanics, 480 ERC, 556-3355 [email protected]

Course Objectives:


1. Conduct experiments that reinforce and verify concepts covered in lecture courses [b]

2. Analyze experimental data and quantitatively evaluate a flow system [b]3. Interpret acquired experimental data/observations through a clear written

technical communication [b]4. Operate a wind tunnel and utilize various pressure probes/liquid manometers

for the measurement of total and static pressure within the flow field, from which be able to compute flow speed [b]

5. Apply the equations of hydrostatics to manometers and understand the implications of static calibration of a pressure transducer [a, b]

6. Investigate the sensitivity of thermal anemometry to setup conditions and flow direction using computer controlled data acquisition. [a, b, k]

7. Calculate the lift and drag on a streamlined body arbitrarily oriented in the flow field through the use of surface measurements [a, b]

8. Calculate the lift and drag on a bluff body using both surface and flow field measurements and applying the conservation of momentum. [a, b]

9. Understand the use of flow obstruction meters for the determination of volume and mass flow rate. [b]

10. Determine through the use of a drag balance the coefficient of drag on generic bluff bodies [a, b]

11. Explain results in a well structured team technical report [d, g]12. Respond to a request to design an experiment to evaluate a pre-specified

fluid dynamic phenomenon using existing laboratory instrumentation and facilities, and present findings orally.

Topics Covered: Fluid Mechanic measurement techniques: Flow speed measurements using pressure probes, velocity measurement using thermal anemometry, volume and mass flow rate determination for internal flows, the measurement of lift and drag on both streamlined and bluff bodies, and the use direct measurement of drag using a force balance.




1, 2, 3, 4, and 6


Application of engineering [a] Hands-on laboratory experience [b] Team environment [d] Enhancement of communication skills [g]



Use of experimental techniques for engineering practice [k]



AEEM 575 Propulsion and Gas Dynamics Laboratory Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-575. Propulsion and Gas Dynamics Laboratory 3 cr. Measurement of pressure, temperature and velocities in flows, force, torque, rotational speed. Nozzle flow, pipe flows with heat addition, compressor and turbine performance parameters/charts. Elements of uncertainty analysis, reporting of data.

Prerequisites: 20-AEEM-329 Engrg Measurements; 20-AEEM-445 Gas Dynamics; 20-AEEM-474 Airbreathing Propulsion

Textbook: Propulsion & Gas Dynamics Laboratory Experiment Notes, S. Jeng/R. DiMicco.References: NoneCoordinator: Peter J. Disimile, Associate Professor of Aerospace Engineering & Engineering

Mechanics, 480 ERC, 556-3355 [email protected] Objectives: The student will be able to

1. Conduct experiments following the guidance of experiment notes and analyze the acquired experimental data with principles of gas dynamics for propulsion devices. [b]

2. Write technical reports describing the laboratory activities. These reports should include: [d, g]

Introduction of experiments, description of experimental apparatus, results of experiments, discussions and comparisons of experimental results with analytical/numerical solutions, conclusions, appendix for raw data and sample calculations

3. Calibrate the pressure and temperature transducers [b]4. Apply gas dynamics principle to calculate the pressure and temperature

history in a discharging chamber and compare to experimental results. [a, e]5. Calculate the one-dimensional compressible flows including effects of

friction, heat addition and variable flow area. [a]6. Measure the performance characteristics of gas turbine propulsion devices and

graphically represent them [b]7. Explain the function and operation of the individual gas turbine components

(fan, compressor, combustor and turbine) 8. Conduct an actual gas turbine performance test and use the thermodynamic

principle to verify the acquired experimental data. [a, b, k]Topics Covered: Experimental method, report preparations and writings, principle and calibration

procedure of pressure transducers and thermocouple, one-dimensional compressible flow, Fanno Flow, Rayleigh Flow, convergent-divergent nozzle, compressor performance chart, turbine performance chart, fan performance chart, flame propagation and stabilization, actual engine thermodynamic cycle and testing.

Computer usage:Prof. Experience: Mathematics; Engineering; General EducationAEEM Program Objectives:

1, 2, 3, 4, and 6


Ability to apply scientific principles [a] Ability to conduct hands-on experiments and interpret data [b, e, k] Ability to communicate results through plots and reports [g] Ability to work in a team environment [d]

AEEM 576 Rocket Propulsion Date Prepared: Feb 2, 2004

Catalog data: 20-AEEM-576. Rocket Propulsion 3 cr. Preliminary design considerations of a rocket engine for a missile or satellite. “Exotic” rocket propulsion systems.

Prerequisites: 20-ENFD-382 Basic Thermodynamics; 20-ENFD-383 Basic Fluid Mechanics;



20-ENFD-385 Basic Heat Transfer; 20-AEEM-445 Gas Dynamics; 20-AEEM-474 Airbreathing Propulsion

Textbook: Rocket Propulsion Elements, G.P. Sutton, Wiley Interscience, 1998References: Space Propulsion Analysis and Design, Ronald W. Humble et al., McGraw-HillCoordinator: Shaaban Abdallah, Professor of Aerospace Engineering & Engineering

Mechanics, 721 Rhodes, 556-3321 [email protected] Objectives: The student will be able to

1. Appreciate rocket history and general operating principles.2. Apply thermodynamic relations for rocket engines and nozzles using the

First and Second Laws of Thermodynamics and the Perfect Gas Law. [a, e]

3. Apply thermal chemistry basics to combustion chambers: absolute and relative enthalpies, heat of formation and reaction, products of combustion using the equilibrium constant method, and flame temperature using the available heat method and chemical kinetics. [a, e, k]

4. Design liquid rocket propulsion systems utilizing preliminary design decisions which include: estimating system mass and envelope; selection of propellant; choice of engine cycle and pressure levels; injection & ignition of liquid propellants [a, c]

5. Perform design trade off studies for thrust chambers and propellant feed system configurations and thrust vectoring [c]

6. Design solid rocket motors utilizing preliminary design decisions which include [a, c, d] component sizing techniques propellant burning rates fuels, oxidizers and binders performance prediction using lumped parameter methods ballistics with variations in spatial pressure calculating specific impulse mass flow and thrust

7. Understand fundamentals of hybrid rocket propulsion systems, nuclear rockets and electric propulsion systems. [a, c, h, j]

8. Identify rocket test procedures. [b]9. Design and test a chemical rocket to meet specified objectives of altitude,

range and flight time. [c]10. Present results as a technical report [g]

Topics Covered: Fundamentals of rocket propulsion system mathematics and equations, component performance and efficiencies, and rocket design procedures.






1, 2, 3, 4, and 5


An ability to apply knowledge of thermodynamics, gas dynamics, & heat transfer [a]

An ability to identify the impact of the mission parameters & their role in engine selection [c, e]

An ability to work with a team and communicate effectively [d, g] Recognition of environmental constraints and their impact on engine

selection [h, j] Use of computer programs to predict combustion properties and rocket

trajectory [k] Ability to identify rocket test procedures [b]



AEEM 597 Composite Structures Date Prepared: February 2, 2004

Catalog data: 20-AEEM-597. Composite Structures. 3 cr. Manufacturing processes of composite materials, design, and analysis of composite structures. Concepts of mechanical and hygro-thermal behavior of composite materials. Properties, strength, and stiffness calculation of composite structures. Application to engineering components

Prerequisites: 20-ENFD-375 Basic Strength of Materials; 20-ENFD-376 Nature & Prop MatlTextbook: Engineering Mechanics of Composite Materials, I. Daniel & O. Ishai, Oxford

University Press, 1994.References: Mechanics of Composite Materials, by R. Christensen, John Wiley and Sons,

1979.Coordinator: Ala Tabiei, Associate Professor of Aerospace Engineering & Engineering


1. Know what composite material means. [j]2. List the difference between the various composite materials. [j]3. Know how composite materials are manufactured. [j]4. Use the macro mechanical behavior models to understand deformation and

elastic response of lamina. [a]5. Determine the properties of fibrous composites. [a, b]6. How to obtain mechanical properties of laminated composites analytically. [a,

e]7. Explain the relationship between constituent properties and laminated

properties. [a]8. Apply micro-mechanics to obtain effective properties of laminated

composites. [a, e]9. Consider the effect of temperature on mechanical properties of composites.

[a]10. Apply failure criteria estimate the strength of composite materials. [a, e]11. Analyze and design composite structural components. [a, c, e]

Topics Covered: Introduction to composite materials, manufacturing composites, mechanics of composite materials, analysis, strength, and design of composite structures.


Engineering


1, 2, 3, 4


Be able to know what composites are [j] How they are manufactured and made [j] Know the appropriate usage and applicability of composite [c] Apply presented formulation to analyze composites [a, e] Design composite parts [b, c]



Appendix I-2.2.Engineering

Fundamentals Course Syllabi



ENFD 101 Mechanics I Date Prepared: February 2, 2004

Catalog data: 20-ENFD-101. Mechanics I. 3 cr. Study of statics – moments, resultant forces, and equilibrium for particles and rigid bodies; friction.

Prerequisites: 15-PHYS-201 Physics I; corequisite 15-MATH-262 Calculus IITextbook: F.P. Beer & E.R Johnston, Vector Mechanics: Statics and Dynamics, 7th ed.;

New Media: McGraw-Hill. (ISBN 007230491X)References: None.Coordinator: James Wade, Associate Professor of Aerospace Engineering & Engineering

Mechanics, 734 RH, 556-3556, [email protected]; Shaaban Abdallah, Professor of Aerospace Engineering & Engineering Mechanics, 721 RH, 556-3321, [email protected].


1. Understand and apply the fundamental concepts and principles of mechanics [a]2. Apply Newton’s laws to a particle body and determine the [a, e]

forces on a particle as vectors resultant of forces resolution of a force into components equilibrium of a particle in two- and three-dimensions

3. Apply Newton’s laws to a rigid body and determine the [a, e] external and internal forces resolution of a given force into a force at a point and couple principle of transmissibility – equivalent forces

4. Determine the conditions of equilibrium of a rigid body [a, e]5. Determine the conditions of equilibrium of multi-rigid body structures [a, e]6. Determine the equilibrium of rigid bodies with friction forces and determine the [a, e]

free-body diagram with friction static and dynamic forces conditions of equilibrium

Topics Covered: The fundamental concepts of the parallelogram law, transmissibility, Newton’s laws and systems of units. Forces on a particle in two- and three-dimensions, resultant of forces in two- and three-dimensions and the equilibrium of a particle body. External and internal forces acting on a rigid body and the equilibrium of a rigid body. Moment about a point and a line. Free body diagram. Analysis of multi-bodies in two- and three-dimensions. Friction and angle of friction. Free body diagram with friction.

Computer usage:Prof. Experience: Mathematics; EngineeringAEEM Program Objectives:

1& 2


Know how to apply mathematical, scientific, and engineering tools from homework and examination [a]

An ability to identify, formulate, and solve engineering problems and ability to draw a free body diagram [a, e]

ENFD 102 Mechanics II Date Prepared: February 2, 2004

Catalog data: 20-ENFD-102. Mechanics II. 3 cr. Development of the fundamental concepts of force and motion in particle dynamics. Applications to a variety of Aerospace, Mechanical, and Civil Engineering problems.



Prerequisites: 20-ENFD-101 Mechanics ITextbook: F.P. Beer & E.R Johnston, Vector Mechanics: Statics and Dynamics, 7th ed.;

New Media: McGraw-Hill. (ISBN 007230491X)References: None.Coordinator: David Richardson, Professor of Aerospace Engineering & Engineering

Mechanics, 730 RH, 556-3365; [email protected] Objectives: The student will be able to

1. Apply [a] Newton’s three laws of particle motion and the Universal Law of

Gravitation. the kinematics of particle motion using Cartesian and cylindrical

coordinates and path variables (in the two-dimensional osculating plane of Serret-Frenet).

basic procedures for Newton’s Second Law to determine equations of motion for dynamical systems of one mass particle.

2. Determine time, speed, position or force information from available dynamical system data. [a, e]3. Formulate procedures using Calculus I and Calculus II combined with [a, e] direct formulations using the Second Law. direct formulations using integrated forms of the Second Law. torque and angular momentum considerations. the principle of work and energy and extensions. the principle of impulse and momentum. Impulsive, non-impulsive,

and average force considerations.4. Compute orbital period, position, and speed. Determine speed change requirements for orbit transfer. [a, e]5. Apply impulse momentum principle in determining two-body collision motions. [a, e]

Topics Covered: Kinematics and coordinate systems, Newton’s Laws, dynamical forces, dynamical equations of motion, integrated forms of the Second Law, elementary orbital motion, two-body impact.




1 & 2



An ability to identify, formulate, and solve engineering problems [a, e]



ENFD 103 Mechanics III Date Prepared: February 2, 2004

Catalog data: 20-ENFD-103. Mechanics III. 3 cr. Centroids, center of gravity. Study of motion and the relationship between force, mass, and acceleration for rigid bodies.

Prerequisites: 20-ENFD-102 Mechanics IITextbook: F.P. Beer & E.R Johnston, Vector Mechanics: Statics and Dynamics, 7th ed.; New

Media: McGraw-Hill. (ISBN 007230491X)References: None.Coordinator: James Wade, Associate Professor of Aerospace Engineering & Engineering

Mechanics, 734 RH, 556-3556, [email protected]; Trevor Williams, Professor of Aerospace Engineering & Engineering Mechanics, 735 RH, 556-3221, [email protected].


1. Analyze the dynamics of a system of particles [a] determine the motion of center of mass compute and use linear and angular momentum, kinetic energy

2. Analyze the kinematics of a rigid body: [a, e] understand translation vs. rotation and angular velocity vectors compute absolute and relative velocities; apply the velocity vector

triangle compute absolute and relative accelerations; motion with and relative to

a rotating frame, including the Coriolis acceleration3. Analyze the planar motion of a rigid body: [a, e, k]

determine the angular acceleration of body, and linear accelerations at all points on it, from the applied forces and moments; moments of inertia; free-body diagrams

apply the work-energy principle to rigid bodies apply the impulse-momentum principle to rigid bodies solve planar rigid body problems involving friction forces; coefficients

of friction; no-slip conditions4. Analyze the general (3-D) dynamics of a rigid body: [a]

understand the inertia tensor; principal axes compute the angular momentum vector and kinetic energy of body Euler’s equations

Topics Covered: Dynamics of systems of particles: momentum, kinetic energy. Kinematics of rigid bodies: relative and absolute velocities and accelerations. Planar motion of rigid bodies: forces and moments; energy and momentum methods. General motion of rigid bodies: Euler’s equations.




1 & 2



An ability to identify, formulate, and solve engineering problems [e] An ability to use the techniques, skills, and modern engineering tools necessary for

engineering practice [k]



ENFD 375 Basic Strength of Materials

Catalog data: 20-ENFD-375. Basic Strength of Materials. 3 cr. Stress-strain curves and properties of materials; direct stress; thermal stress; shear; torsion; flexure; deflections of beams; columns; combined stresses.

Prerequisites: Calculus and Analytical Geometry III (15-MATH-264)

Textbook: Beer, Johnston & DeWolf, Mechanics of Materials, 3rd Ed., McGraw-Hill

References: Gere & Timoshenko, Mechanics of Materials, 4th Ed., Brooks/Cole

Coordinator: Dr. James A. Swanson, Assistant Professor of Civil Engineering

Goals: This course introduces the basic topics of structural analysis. The goal is to enable the students to solve elastic problems involving any external loading, with particular focus on the calculation of stresses and deformations.

Lecture or lab topics:

1. Review of static’s. Internal forces. (1 class)2. Review of approaches to the solution of trusses (1 class)3. The concepts of normal stress and shear stress (2 classes)4. Stress-strain curves. Definition of normal strain (2 class)4. Uniaxial, biaxial, triaxial states of stress. Definition of shearing stress.

Hooke’s Law for the general case. (2 classes)5. Statically determinate and indeterminate structures subjected to axial forces.

Temperature effects. (3 classes)6. Effects of torque on structures. Shearing stress and angle of twist (2 classes)7. Statically determinate and indeterminate structures subjected to torque.

Interaction of gears (2 classes)8. Transversally loaded beams. Internal shear and internal moment. Diagrams.

(2 class)9. Normal stress due to bending moment (2 classes)10. Shear stress due to shear (2 classes)11. Relationship between external load, shear and moment. Internal force

diagrams (3 classes)12. Design of beams for normal stress and shear stress (1 class)13. Stress transformation. Analytical and graphical approach (Mohr’s circle)(2

classes).14. Midterms and final exam. (2 classes)

Computer usage: Due to the mostly theoretical content of the course, and to the relatively simple problems, the usage of computer programs is limited. General mathematic programs can be used to solve simple differential equations or to calculate solutions to elementary integrals or linear systems of equations.

ABET Criteria 3: a, c, e

Date prepared: March 2, 2004



Specific Examples of ABET Criteria 3a: The assigned homework covers a wide range of problems associated with the theoretical topics analyzed in class, and include problems for the solution of which a moderate level of engineering judgment is required. The solution of the proposed problems requires extensive use of the mathematics and calculus background of the students, as well as ingenuity and intuition.

c: The covered topics and the assigned homework explicitly involve the design and/or the verification of a simple structural system or of an assembly of simple structural systems, including the design process necessary in order to obtain a structure compatible with given deformability or stress constraints.

e: The very nature of the topics covered by the course requires the students to become able to identify, formulate and solve the given structural problems.

Specific Examples of ABET Criteria 8a: Basic knowledge of trigonometry, analytic geometry, linear algebra and calculus are necessary for the solution of the vast majority of the problems assigned during the course, and the students need to apply all these theoretical topics on practical problems.

d: The topics taught in this course will allow the students to be able to actively participate in the design process possibly involved in the professional component of the curriculum.



ENFD 382 Basic Thermodynamics

Catalog data: ENFD-382-001 Basic Thermodynamics 3 cr.

Prerequisites: none

Textbook: Y.A. Cengel and M.A. Boles, Thermodynamics- An Engineering Approach, 4th ed., McGraw-Hill, 2002

References: none

Coordinator:

Goals: The goal of this course is to teach the key concepts of thermodynamics, through the investigation of examples and introduction to the principles. The course will focus on the development of ideas and problem solving techniques.

Lecture or lab topics:

1. Basic concepts of thermodynamicsa) Dimensions and Unitsb) Closed and Open Systemsc) Energyd) Pressure

2. Properties of Pure substancesa) Phase Changes Processesb) Phase Diagramsc) Equation of State d) Specific Heats e) Internal Energy, Enthalpy, and Specific Heats of Ideal Gas, Solids and Liquids

3. Energy Transfer by Heat, Work and Massa) Heat Transferb) Energy Transfer by Workc) Forms of Workd) Conservation of Mass Principle

4. The First Law of Thermodynamicsa) The First Law of Thermodynamicsb) Energy Balance for Closed Systemsc) Energy Balance for Steady Flow Systemsd) Some Steady Flow Engineering Device5. The Second Law of Thermodynamicsa) Thermo Energy Reservoirsb) Heat Enginesc) Energy Conversion Efficienciesd) Refrigerators and Pumpse) The Carnot CycleMidterms and final exam. (2 classes)

Computer usage: none

ABET Criteria 3: a, c, e

Date prepared: May 2, 2004



Specific Examples of ABET Criteria 3a: The assigned homework covers a wide range of problems associated with the theoretical topics analyzed in class, and include problems for the solution of which a moderate level of engineering judgment is required. The solution of the proposed problems requires extensive use of the mathematics and calculus background of the students, as well as ingenuity and intuition.

c: The covered topics and the assigned homework explicitly involve the design and/or the verification of a simple structural system or of an assembly of simple structural systems, including the design process necessary in order to obtain a structure compatible with given deformability or stress constraints.

e: The very nature of the topics covered by the course requires the students to become able to identify, formulate and solve the given structural problems.

Specific Examples of ABET Criteria 8a: Basic knowledge of trigonometry, analytic geometry, linear algebra and calculus are necessary for the solution of the vast majority of the problems assigned during the course, and the students need to apply all these theoretical topics on practical problems.

d: The topics taught in this course will allow the students to be able to actively participate in the design process possibly involved in the professional component of the curriculum.



ENFD 383 Basic Fluid Mechanics Date Prepared: Feb 2, 2004

Catalog data: 20-ENFD-383. Basic Fluid Mechanics. 3 cr. Physical nature of fluids, fluid statics, conservation principles and their application to engineering problems. Bernoulli equation. Duct flow of real fluids with losses.

Prerequisites: 15-MATH-254 Calculus IV; 15-MATH-273 Differential Equations; 20-ENFD-101 Mechanics I

Textbook: Introduction to Fluid Flow, R. W. Fox & A. T. McDonaldWiley Publishing Co., 5th ed.

References: Fluid Flow—A First Course in Fluid Mechanics, Sabersky & Acosta,MacMillan

Coordinator: Kirti (Karman) Ghia, Professor of Aerospace Engineering & Engineering Mechanics, 681 RH, 556-3243, [email protected]


1. Define a continuous fluid and flow behavior at a point [a]

2. Apply the equilibrium principle to solve simple hydrostatic and manometer problems. [a, e]3. Apply integral conservation laws of mass and momentum to control volumes [a, e]

4. Apply the continuity equation for possible fluid flow [a]

5. Solve for the stream lines, path lines, and streak lines [a, k]

6. Apply Bernoulli equation [e]

7. Application to pipe flows with and without losses [e, k]Topics Covered: Observable fluid properties and introductory concepts. Basic integral

conservation laws of mass and momentum. Apply to hydrostatics. Differential approach and Bernoulli equation. Application to pipe flows with and without losses.




1 & 2


Ability to apply mathematics, science, and engineering principles to problem solving [a]

Ability to identify the role of appropriate control volumes, stream lines, and engineering approximations to problem solving [e, k]



ENFD 385 Basic Heat Transfer

Catalog data:20-ENFD-385. Basic Heat Transfer. 3 Cr. Fundamental concepts of heat transfer including conduction, convection and radiation.

Prerequisites: 15-MATH-273 Differential Equations (Recommended)

Textbook: J. P. Holman, Heat Transfer, 9th Ed., McGraw-Hill

References: None

Coordinator: Daniel Hershey, Professor, Chemical Engineering


Understand the mechanisms of conduction, convection, and radiation

Solve simple steady – and unsteady – state conduction problems in several configurations

Understand the fundamentals of convective transfer

Design simple double-pipe exchangers and understand simple heat exchangers

Solve radiation problems in conjunction with convection and conduction

Topics Covered: 1. Steady – and unsteady – state conduction and convection .2. Heat exchangers. Introduction of pertinent concepts of fluid

mechanics, and equations of energy conservation .3. Radiation and radiation combined with conduction and/or

convection

Computer usage:General mathematic programs can be used to solve simple equations or to calculate solutions.

Professional Experience:ABET Criteria Addressed:

a, c, e

Date prepared: June 3, 2004


I-2 - University of Cincinnatiprogram/program/ABET_I-2_syllabi.doc · Web viewEngineering Fundamentals Course Syllabi I-2 Page 44 Appendix I-2.1. Aerospace Engineering Course Syllabi

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