GATE AE 2025 • Q28 MCQ • 1 Mark Aerospace Structures

Aerospace Structures

Strength of Materials & Elasticity

Subtopic: Stress and Strain Tensors & Generalized Hooke's Law

Question Statement:

A stress field is given by $\sigma_{xx} = \sigma_{zz} = C_1y$; $\sigma_{yy} = C_2y$; $\tau_{xy} = \tau_{yz} = \tau_{zx} = 0$, where $C_1$ and $C_2$ are non-zero constants. If the stress field satisfies equilibrium, which one of the following options is correct?

Options:

  • (A) There is no body force per unit volume.
  • (B) There is a constant body force per unit volume in the y-direction.
  • (C) The body force per unit volume varies linearly in the y-direction.
  • (D) The direction of the body force per unit volume depends on the value of C1.

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2025 Q.28)** **1. Intuitive Physical Setup & Given Parameters**: Given stress field in a 3D Cartesian continuum: - Normal stresses: $\sigma_{xx} = C_1 y$, $\sigma_{yy} = C_2 y$, $\sigma_{zz} = C_1 y$ - Shear stresses: $\tau_{xy} = 0$, $\tau_{yz} = 0$, $\tau_{zx} = 0$ - $C_1, C_2 \neq 0$ are non-zero constants. We are given that the stress field satisfies the static equilibrium equations: \frac{\partial \sigma_{ji}}{\partial x_j} + B_i = 0 We need to determine the characteristics of the body force per unit volume $\vec{B} = (B_x, B_y, B_z)$. **2. Step-by-Step Continuum Mechanics Derivation**: 1. **Equations of Equilibrium in Cartesian Coordinates**: - Along $x$-direction: \frac{\partial \sigma_{xx}}{\partial x} + \frac{\partial \tau_{yx}}{\partial y} + \frac{\partial \tau_{zx}}{\partial z} + B_x = 0 \frac{\partial (C_1 y)}{\partial x} + 0 + 0 + B_x = 0 \implies 0 + B_x = 0 \implies B_x = 0 - Along $z$-direction: \frac{\partial \tau_{xz}}{\partial x} + \frac{\partial \tau_{yz}}{\partial y} + \frac{\partial \sigma_{zz}}{\partial z} + B_z = 0 0 + 0 + \frac{\partial (C_1 y)}{\partial z} + B_z = 0 \implies 0 + B_z = 0 \implies B_z = 0 - Along $y$-direction: \frac{\partial \tau_{xy}}{\partial x} + \frac{\partial \sigma_{yy}}{\partial y} + \frac{\partial \tau_{zy}}{\partial z} + B_y = 0 0 + \frac{\partial (C_2 y)}{\partial y} + 0 + B_y = 0 C_2 + B_y = 0 \implies B_y = -C_2 2. **Analysis of the Body Force Vector**: - $B_x = 0$, $B_z = 0$, and $B_y = -C_2 = \text{constant}$. - Because $C_2$ is a non-zero constant, there is a **constant body force per unit volume in the $y$-direction**. - Note that $B_y$ is completely independent of $C_1$ and spatial coordinates $(x, y, z)$. **3. Comprehensive Options & Distractor Analysis**: - **(A) There is no body force per unit volume**: ❌ **INCORRECT**. Requires $\frac{\partial \sigma_{yy}}{\partial y} = 0$, but $\frac{\partial (C_2 y)}{\partial y} = C_2 \neq 0$. - **(B) There is a constant body force per unit volume in the y-direction**: ✅ **CORRECT**. $B_y = -C_2 = \text{const}$, $B_x = B_z = 0$. - **(C) The body force per unit volume varies linearly in the y-direction**: ❌ **INCORRECT**. The derivative of a linear function is constant. - **(D) The direction of the body force per unit volume depends on the value of C1**: ❌ **INCORRECT**. Depends solely on $C_2$. **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **B** - **Exam Takeaway**: Differential equilibrium requires $B_i = -\partial \sigma_{ji}/\partial x_j$. Differentiating $\sigma_{yy} = C_2 y$ yields constant body force $B_y = -C_2$.
← Previous (Q27) All 2025 Questions Next (Q29) →

Related Strength of Materials & Elasticity Solved Questions

View All Strength of Materials & Elasticity PYQs →
GATE AE 2026 Q12 MCQ • 1M

The Fourier series representation of a square wave is shown in the figure below. The fluctuations seen near x = ±1 are named after which one of the following scientists?

GATE AE 2026 Q40 MCQ • 2M

Consider a unit square body as shown in the figure below. The body is subjected to the deformation field u = -ay and v = ax, where 'a' is a constant. Due to the application of this deformation field, the body undergoes _______ in the x-y plane.

GATE AE 2026 Q45 MSQ • 2M

The deformation of an open-section bar subjected to pure torsion can be solved by choosing an appropriate Prandtl stress function. Which of the following statements is/are true about the Prandtl stress function?

GATE AE 2026 Q57 NAT • 2M

WA and WB are the respective maximum take-off weights of an aircraft for two ambient air conditions given below. Condition A: p = 1 bar, T = 50 oC; Condition B: p = 0.66 bar, T = -30 oC If all other parameters relevant for take-off are kept the same in these two conditions, the ratio WB/WA is ________ (rounded off to 3 decimal places).

Practice This in Real CBT Exam Interface

Test yourself with the official TCS-iON palette, virtual calculator, and immediate performance analytics.

Launch CBT Mock Test