Question: Lecture 2 0 Matrix methods for Uniform Combined Axial & Shear Stress & Strain, True Strain, and PDEs for Static Equilibrium Problem 2 0 .

Lecture 20 Matrix methods for Uniform Combined Axial & Shear Stress & Strain, True Strain, and PDEs for Static Equilibrium
Problem 20.1
Suppose a large rectangular prism is made of an elastic material with E=80MPa (note: MPa not GPa ) and v=0.4 and has dimensions Lx=1m,Ly=1m, and Lz=2m, extending from one corner at the origin to an opposite corner at (Lx,Ly,Lz). The prism is put into a uniform shear stress & strain condition by applying appropriate normal and shear forces on its external faces so that the internal axial stress vector is =(0,0,40kPa) and the internal shear stress vector is =(:yz,xz,xy:)=(:0,40kPa,0:).
If the corner at the origin is fixed in place and the z -displacement of the entire z=0 surface is 0(i.e., the surface can't rotate in any direction or translate in z ), find an expression for the x-,y-, and z -displacement of the prism induced by this loading at any point in the prism.
Hint: with axial and shear strain happening at once, displacement in the x-direction due to strain is (from a total derivative, with small strains)du=deludelxdx+deludelydy+deludelzdz
If the partial derivatives are constant over the whole object (as they would be in a uniform strain situation), then integrating gives: u=deludelxx+deludelyy+deludelzz, i.e.,
u(x,y,z)-u(x0,y0,z0)=deludelx(x-x0)+deludely(y-y0)+deludelz(z-z0)
and similarly for v and w.
Hint 2: In your answer, explain why this set of equations
{[du=deludelxdx+deludelydy+deludelzdz],[dv=delvdelxdx+delvdelydy+delvdelzdz],[dw=delwdelxdx+delwdelydy+delwdelzdz]}
simplifies to {[du=xdx+zxdz],[dv=ydy],[dw=zdz]}; in particular, explain why there's no xzdx contribution to dw
Lecture 2 0 Matrix methods for Uniform Combined

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