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Chapter 4 Deflection-f (1)

Feb 28, 2018

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    Mechanical Design I (MCE 321) L. Romdhane, SS 2016, 11:33 AM -- 1--

    Summer 2016

    Chapter 4Deflection and Stiffness

    Mechanical Design 1(MCE 321)

    Dr. Lotfi

    Romdhane

    [email protected]

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    Chapter Outline

    4-1 Spring Rates

    4-2 Tension, Compression, and Torsion

    4-3 Deflection Due to Bending

    4-4 Beam Deflection Methods

    4-5 Beam Deflections by Superposition

    4-6 Beam Deflections by Singularity Functions

    4-7 Strain Energy

    4-8 Castiglianos Theorem

    4-9 Deflection of Curved Members

    4-10 Statically Indeterminate Problems

    4-11 Compression MembersGeneral

    4-12 Long Columns with Central Loading

    4-13 Intermediate-Length Columns with Central Loading

    4-14 Columns with Eccentric Loading

    4-15 Struts or Short Compression Members

    4-16 Elastic Stability

    4-17 Shock and Impact

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    Spring Rates

    A spring is a mechanical element that exerts a forcewhen deformed.

    If we designate the general relationship between forceand deflection by the equation

    then spring rate is defined as

    where y must be measured in the direction of F and atthe point of application of F.

    For linear force-deflection problems, k is a constant,also called the spring constant

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    Tension, Compression, and Torsion

    The total extension or contraction of a uniform bar inpure tension or compression, is given by

    The spring constant of an axially loaded bar is then

    The angular deflection of a uniform round barsubjected to a twisting moment Tis

    where is in radians

    The torsional spring rate is

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    Deflection Due to Bending

    The curvature of a beam subjected to a bendingmoment M is given by

    where is the radius of curvature

    The slope of the beam at any pointxis

    Therefore

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    Deflection Due to Bending

    (410)

    (411)

    (412)

    (413)

    (414)

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    Beam Deflection Methods

    There are many techniques employed to solve

    the integration problem for beam deflection.

    Some of the popular methods include :

    Superposition

    Singularity functions

    Energy

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    Example 1: Superposition

    Beam Deflections bySuperposition :Superpositionresolves the effect ofcombined loading on a structure bydetermining the effects of each load

    separately and adding the resultsalgebraically.

    +

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    Example 42 (continued)

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    Example 2: Superposition

    +

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    Example 2: Superposition

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    Example 2: Superposition

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    Example 2: Superposition

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    Tables

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    For tension and compression

    The strain energy for torsion isgiven by

    The strain energy due to directshear

    Strain Energy

    The external work done on an elastic

    member in deforming it, is transformed

    into strain, or potentialenergy.

    The energy is equal to the product of the

    average force and the deflection, or

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    Strain Energy due to

    Bending and shear loading

    The strain energy storedin a section of the elasticcurve of length ds is

    =

    2 =

    2

    For small deflections,

    = and

    =

    . Then,for the entire beam

    Summarized to includeboth the integral andnon integral form, thestrain energy for bending is

    The strain energy dueto shear loading of abeam can beapproximated as

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    Example 1: Strain Energy

    Determine the

    strain energy for the

    simply supported

    beam

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    Example 2: Strain Energy

    A

    B

    P

    R

    Determine the BendingStrain Energy for the

    curved beam

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    Castiglianos Theorem

    Castiglianos theorem states that

    when forces act on elastic systems subject to small displacements, the

    displacement corresponding to any force, in the direction of the force, is

    equal to the partial derivative of the total strain energy with respect to

    that force.

    where i is the displacement of the point of application of the force Fiin the direction of Fi

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    Castiglianos Theorem (applications)

    Castiglianostheorem can be used to find the deflection at a

    point even though no force or moment acts there.

    Set up the equation for the total strain energy U

    Find an expression for the desired deflection

    Since Q is a fictitious force, solve the expression by setting Q equal to zero.

    Tension/ Compression

    2

    2

    F L FL

    F AE AE

    2

    2T L TL

    T GJ GJ

    Torsion

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    Castiglianos Theorem (applications)

    2 3 3

    8 4A

    P R PRy

    P EI EI

    P

    A

    B

    R

    Bending (Shear Contributions)

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    Example 410

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    Example 410 (continued)

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    Example 410 (continued)

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    Example 410 (continued)

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    Example 3: Castiglianos Theorem

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    Long Columns with Central Loading

    If the axial force P shown acts along thecentroidal axis of the column, simplecompression of the member occurs for lowvalues of the force.

    Under certain conditions, when P reaches a

    specific value, the column becomesunstable and bending develops rapidly.

    The critical force for the pin-endedcolumn is given by

    which is called the Euler column formula

    Euler Column formula can be extended to applyto other end-conditions by writing

    where the constant C depends on the end conditions

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    Long Columns with Central Loading

    Critical Buckling Load

    2

    2cr

    C EIP

    l

    2I Ak2

    2cr

    P C E

    A l

    k

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    Euler Column Formula : General

    Using the relation = 2, whereis the area and the radius of

    gyration. Euler Column Equation can be rearranged as

    where

    is called the slenderness ratio

    The quantity

    is the critical unit load. It is the load per unit areanecessary to place the column in a condition of unstable equilibrium.

    The factor C is called the

    end-condition constant,

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    Euler Column Formula : Application

    In practical engineering applications where defects such as initialcrookedness or load eccentricities exist, the Euler equation can only be

    used for slenderness ratio greater than

    Most designers select point T such that

    =

    with corresponding

    value of

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    Euler Column Formula : Example

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    Columns with Eccentric Loading

    The magnitude of the maximum compressive

    stress at mid span is found by superposing theaxial component and the bending component.

    By imposing the compressiveyield strength as the

    maximum value of

    The term

    is called the

    eccentricity ratio.

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    Struts or Short Compression Members

    A strut is a short compression member such thatthe maximum compressive stress in thex directionat point B in an intermediate section is the sum of asimple component P/A and a flexural componentMc/I

    where =

    is the radius of gyration, is the

    coordinate of point B, and is the eccentricity ofloading.

    How long is a short member?

    If we decide that the limiting percentage is to be 1percent of , then, the limiting slenderness ratioturns out to be

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    Summary

    =

    1 +

    Struts

    Short columnsIntermediate

    length columnsLong columns