GATE AE 2022 • Q60 NAT • 2 Marks Aerospace Structures

Aerospace Structures

Strength of Materials & Elasticity

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

Question Statement:

A $10\text{ kN}$ axial load is applied eccentrically on a rod of square cross-section ($1\text{ cm} \times 1\text{ cm}$) as shown in the figure. The strains measured by the two strain gages attached to the top and bottom surfaces at a distance of $0.5\text{ m}$ from the tip are $\epsilon_1 = 0.0016$ and $\epsilon_2 = 0.0004$, respectively. The eccentricity in loading, $e$, is ______ $\text{mm}$.

Official Answer Key:

1.0

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2022 Q.60)** **1. Combined Axial and Bending Strain**: $$\epsilon_1 = \frac{P}{AE} + \frac{P e (c)}{I E}, \quad \epsilon_2 = \frac{P}{AE} - \frac{P e (c)}{I E}$$ Sum and difference: $$\epsilon_1 - \epsilon_2 = \frac{2 P e c}{I E}, \quad \epsilon_1 + \epsilon_2 = \frac{2P}{AE}$$ Dividing the two relations: $$\frac{\epsilon_1 - \epsilon_2}{\epsilon_1 + \epsilon_2} = \frac{e c A}{I}$$ For square section of side $a = 1\text{ cm} = 10\text{ mm}$: $$c = \frac{a}{2}, \quad I = \frac{a^4}{12}, \quad A = a^2 \implies \frac{c A}{I} = \frac{a/2 \cdot a^2}{a^4/12} = \frac{6}{a}$$ $$\frac{0.0016 - 0.0004}{0.0016 + 0.0004} = \frac{0.0012}{0.0020} = 0.6 = \frac{6 e}{10\text{ mm}} \implies e = 1.0\text{ mm}$$ - **Official Answer Key**: **1.0**
← Previous (Q59) All 2022 Questions Next (Q61) →

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