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Summer 2016
Chapter 4Deflection and Stiffness
Mechanical Design 1(MCE 321)
Dr. Lotfi
Romdhane
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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