22-Mec-A7 Advanced Strength of Materials · December 2014
Question 3 of 8: Strain compatibility and integration of a plane strain field
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams — December 2014, 07-Mec-A7 Advanced Strength of Materials. Open-book, 3 hours; any five of the eight problems constitute a complete paper and all problems are of equal value. All eight problems are solved as a study resource.
Given. The plane strain components $\varepsilon_x=c(-3x^2+7y^2)$, $\varepsilon_y=c(x^2-5y^2)$, $\gamma_{xy}=bxy$.
Find. (a) the compatibility relation between b and c; (b) the displacements at (1, 5) with the origin fixed and b = 5.
Approach. Enforce the 2-D compatibility equation, then integrate the strain–displacement relations, fixing the rigid-body constants at the origin.
Compatibility (part a). The single 2-D compatibility condition is
$$\frac{\partial^2\varepsilon_x}{\partial y^2}+\frac{\partial^2\varepsilon_y}{\partial x^2}=\frac{\partial^2\gamma_{xy}}{\partial x\,\partial y}.$$
Here $\partial^2\varepsilon_x/\partial y^2=14c$, $\partial^2\varepsilon_y/\partial x^2=2c$, and $\partial^2\gamma_{xy}/\partial x\partial y=b$, so
$$14c+2c=b\;\Rightarrow\;\boxed{b=16c}$$
Integrate the direct strains. From $\varepsilon_x=\partial u/\partial x$ and $\varepsilon_y=\partial v/\partial y$,
$$u=c\!\left(-x^3+7y^2x\right)+f(y),\qquad v=c\!\left(x^2y-\tfrac{5}{3}y^3\right)+g(x).$$
Enforce the shear strain. Substituting into $\gamma_{xy}=\partial u/\partial y+\partial v/\partial x=16cxy+f'(y)+g'(x)$ and equating to $bxy=16cxy$ gives $f'(y)+g'(x)=0$. With no rigid-body rotation and $u(0,0)=v(0,0)=0$, all constants vanish, so $f=g=0$.
Evaluate at (1, 5) with b = 5. Then $c=b/16=0.3125$ and
$$u(1,5)=c(-1+7\cdot25)=174c=\boxed{54.4},\qquad v(1,5)=c\!\left(5-\tfrac{5}{3}\cdot125\right)=-203.3c=\boxed{-63.5}$$
(in the same length units as the coordinates).