Introduction to Aerospace Engineering
Octavian Thor Pleter, PhD, PhD, MBA (MBS)
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This presentation draws on ideas from Dr. Pleters articles, books, and unpublished manuscripts. No part of this publication may be reproduced, stored in a retrieval system or transmitted by any means or in any form - electronic,
mechanical, photocopying, recording or otherwise - without written consent from Octavian Thor Pleter or the
Brainbond consultancy firm, www.brainbond.ro Version 1.0 dated 23 October 2009 O. T. Pleter and Brainbond
Course Outlines
1. Introduction. Why Aerospace Engineering?
2. Flight Principles. Classification of Aircraft and Spacecraft.
3. Airplane. Aircraft Structure and Systems. Flight Control.
4. Aircraft Classes and Categories. Aircraft Materials.
5. Airplane Flight. Lift, Weight, Thrust, Drag. Airfoils.
6. Axes. Controls, Stability. Load Factor. Stall.
7. Helicopters. Controls, Stability. Lighter than Air Aircraft.
8. Airspeed, Mach Number. Flight Instruments: Pitot, Gyro, Magnetic.
9. Aero Engines and the Fuel System. Piston Engine. Jet Engine.
Instruments.
10.Aerodrome Operations. Air Traffic Management, Airspace. VFR, IFR.
11.Spacecraft Propulsion, Control and Stability.
12.Navigation. Air Navigation Systems. Automatic Flight Control. FMS.
13.Air Transport Engineering. Aviation Business. Regulators. Chicago
Convention.
14.Conclusions.
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Archytas of Tarentum in 400 B.C. invented the pulley, the screw, a
flying wooden pigeon (probably an aerodyne), and the kite.
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Kite Flight Dynamics
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Aerodynamic Forces
20/ 2
LL V S C
20/ 2
DD V S C
Lift
Drag
Air Density
Airspeed
Wing Surface
Lift Coefficient
Drag Coefficient
Useful Subjects: Fluid Dynamics / Aerodynamics
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aerodynamic forces are measured in the wind tunnel
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Kite Wing Polar
Useful Subjects: Fluid Dynamics / Aerodynamics
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Problem: Design your own kite
Choose:
WS = wing span
l = length material (e.g. cardboard) place where you launch (e.g. Bucharest)
Calculate:
m = mass W = weight best L = lift D = drag T = thrust
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Problem: Design your own kite
Choose:
WS = 0.8 m
l = 1.2 m material: CO5 cardboard 820 g/m2
place where you launch: Bucharest (close to sea level) wind speed to raise the kite V = 8 m/s
Calculate:
S = l WS = 1.2 0.8 = 0.96 m2
m = 0.82 kg 0.96 m2 = 0.787 kg W = mg = 0.787 kg 9.81 m/s2 = 7.72 N + 6.28 N rope + tail = 14 N best = 12 L = 1.225 kg/m3 / 2 82 0.96 m2 0.68 = 25.59 N
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Problem: Design your own kite
Continue calculate:
D = 1.225 kg/m3 / 2 82 0.96 m2 0.44 = 16.56 N
solve the right triangle with two sides:
LW = 25.59 14 = 11.59 N
D = 16.56 N
b = arctan ((L W)/D) = 35
T = ((L W)2+D2) = 20.21 N
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2
2 2 cos4 2
Va c c b
Useful Subjects: Geometry
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2 2
2 2 cos4 2 4
WSa c c b
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2 2
2 2 cos 1804 2 4
WSb c c b
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Problem: Design your own kite
Choose c = 1 m
Continue calculate:
a = 0.838 m
b = 1.529 m
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Problem: Design your own kite
Data inputs:
shape: diamond
material: balsa wood 1.8 g/m and tissue 12.5 g/m2
place where you launch: Bucegi Plateau (2000 m altitude)
wind speed to raise the kite V = 5 m/s
weight of rope and tail = 6 N
best = 12
Useful Subjects: Aircraft Materials / Atmosphere Physics
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Drag of a Disc
Useful Subjects: Fluid Dynamics / Aerodynamics
Turbulence volume:
the vortices at the front and at the back drag the
disc behind, like a parachute
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Drag of a Water Drop - Shaped Body
Useful Subjects: Fluid Dynamics / Aerodynamics
Fill the volume of the turbulence volume with material
the vortices have no more room
the turbulence disappears; flow is laminar
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Aurel Persu
Romanian Professor of Politehnica University of Bucharest
In 1923 invented the first aerodynamic car
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Types of Drag
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Problem: What is the best shape for a braking parachute?
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Wing = Maximum Lift for Minimum Drag
Useful Subjects: Fluid Dynamics / Aerodynamics
water drop cross section
kite-style flat rectangle
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Symmetric Airfoil Zero Incidence
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Cambered Airfoil Positive Incidence
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Turbulence Volume for a Kite
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Fill the Turbulence Volume with Material
Spectacular reduction in drag
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Cambered Airfoil
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Flight = Balance of 4 Forces
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Useful Subjects: Flight Dynamics