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Application Solutions of Plane Elasticity
Professor M. H. Sadd
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Solutions to Plane Problems Cartesian Coordinates
Airy Representation Biharmonic Governing Equation R S Traction Boundary Conditions x y
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Uniaxial Tension of a Beam
y T 2l 2c
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Note Integrated Boundary Conditions
Pure Bending of a Beam x y M 2l 2c Note Integrated Boundary Conditions
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Bending of a Beam by Uniform Transverse Loading
x y w 2c 2l wl x/w - Elasticity x/w - Strength of Materials l/c = 2 l/c = 4 l/c = 3 Dimensionless Distance, y/c
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Bending of a Beam by Uniform Transverse Loading
x y w 2c 2l wl Note that according to theory of elasticity, plane sections do not remain plane For long beams l >>c, elasticity and strength of materials deflections will be approximately the same
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Cantilever Beam Problem
x y N P L 2c Stress Field Displacement Field
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Cantilever Tapered Beam
x y L p A B Stress Field x = L x = L
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Solutions to Plane Problems Polar Coordinates
Airy Representation Biharmonic Governing Equation R S Traction Boundary Conditions x y r
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General Solutions in Polar Coordinates
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Thick-Walled Cylinder Under Uniform Boundary Pressure
r1/r2 = 0.5 r/r2 r /p /p Dimensionless Distance, r/r2 Internal Pressure Case
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Stress Free Hole in an Infinite Medium Under Uniform Uniaxial Loading at Infinity
r/a
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Stress Concentrations for Other Loading Cases
Biaxial Loading T Biaxial Loading T Unaxial Loading K=3 K=2 K=4
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Stress Concentration Around Elliptical Hole
x y b a ()max/S Circular Case (K=3)
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Half-Space Under Concentrated Surface Force System (Flamant Problem)
x y Y X r C Normal Loading Case (X=0) Dimensionless Distance, x/a y/(Y/a) xy/(Y/a) y = a
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Notch-Crack Problems Contours of Maximum Shear Stress y r x
= 2 - r x Contours of Maximum Shear Stress
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Two-Dimensional FEA Code MATLAB PDE Toolbox
- Simple Application Package For Two-Dimensional Analysis Initiated by Typing “pdetool” in Main MATLAB Window Includes a Graphical User Interface (GUI) to: Select Problem Type Select Material Constants Draw Geometry Input Boundary Conditions Mesh Domain Under Study Solve Problem Output Selected Results
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FEA Notch-Crack Problem
(vonMises Stress Contours)
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Curved Beam Problem P r a b = /2 b/a = 4 a/P
Dimensionless Distance, r/a a/P Theory of Elasticity Strength of Materials = /2 b/a = 4
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Disk Under Diametrical Compression
= P Flamant Solution (1) + + Flamant Solution (2) Radial Tension Solution (3)
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Disk Under Diametrical Compression
+ + = P 2 y x 1 r1 r2
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Disk Results Theoretical, Experimental, Numerical
Theoretical Contours of Maximum Shear Stress Finite Element Model (Distributed Loading) Photoelastic Contours (Courtesy of Dynamic Photomechanics Laboratory, University of Rhode Island)
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