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22-Mec-A7 Advanced Strength of Materials · May 2015

Question 4 of 8: Strain State from a Prescribed Displacement Field

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. National Exams, May 2015 — 07-Mec-A7 Advanced Strength of Materials. Open-book, 3 hours. Eight problems of equal value; any five constitute a complete paper. All eight are solved here.

Reference texts. Ugural & Fenster, Advanced Strength and Applied Elasticity (4th ed.); Boresi & Schmidt, Advanced Mechanics of Materials (6th ed.); Hibbeler, Mechanics of Materials (10th ed.); Timoshenko & Goodier, Theory of Elasticity.

Question 4: Strain State from a Prescribed Displacement Field (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. Corner A at (1.0, 1.5, 2.0) m moves to A′(0.9955, 1.4982, 1.9997) m under $u=c_1xyz$, $v=c_2xyz$, $w=c_3xyz$.

Find. (a) the six strain components at A; (b) the normal strain along AB; (c) the shear strain between the perpendicular lines AB and AC.

ABCA'1.5 m (y)2.0 m (z)1.0 m (x)
Block with corner A (1,1.5,2); AB is the front-face diagonal to B(1,0,0) and AC is the top edge to C(0,1.5,2); AB ⊥ AC.

Approach. Fit the three constants from A’s displacement, differentiate the field for the small-strain components, then use the strain-transformation quadratic forms with the unit vectors of AB and AC.

  1. Constants of the field. The displacement of A is $(-0.0045,-0.0018,-0.0003)$ m and $xyz=3.0$ at A, so $$c_1=-1.5\times10^{-3},\quad c_2=-0.6\times10^{-3},\quad c_3=-0.1\times10^{-3}.$$
  2. (a) Strain components. Differentiating and evaluating at A(1, 1.5, 2), $$\varepsilon_x=c_1yz,\ \varepsilon_y=c_2xz,\ \varepsilon_z=c_3xy,\quad \gamma_{xy}=c_1xz+c_2yz,\ \gamma_{xz}=c_1xy+c_3yz,\ \gamma_{yz}=c_2xy+c_3xz,$$ giving $\varepsilon_x=-4500\mu$, $\varepsilon_y=-1200\mu$, $\varepsilon_z=-150\mu$, $\gamma_{xy}=-4800\mu$, $\gamma_{xz}=-2550\mu$, $\gamma_{yz}=-1100\mu$.
  3. (b) Normal strain along AB. With $\mathbf{n}_{AB}=(0,-0.6,-0.8)$, $$\varepsilon_{AB}=\varepsilon_y n_y^2+\varepsilon_z n_z^2+\gamma_{yz}n_yn_z=\boxed{-1056\ \mu\varepsilon}.$$
  4. (c) Shear strain between AB and AC. With $\mathbf{n}_{AC}=(-1,0,0)$ (and $\mathbf{n}_{AB}\cdot\mathbf{n}_{AC}=0$), $$\gamma_{AB,AC}=2\,\mathbf{n}_{AB}^{\mathsf T}[\varepsilon]\,\mathbf{n}_{AC}=\boxed{-4920\ \mu\varepsilon}.$$ The originally-right angle between AB and AC opens (positive relative rotation would close it), by 4920 microradians.
Final results — Question 4
QuantityValue (με)
εx, εy, εz−4500, −1200, −150
γxy, γxz, γyz−4800, −2550, −1100
Normal strain along AB−1056
Shear strain AB–AC−4920