GATE AE 2025 • Q59 NAT • 2 Marks Aerospace Structures

Aerospace Structures

Strength of Materials & Elasticity

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

Question Statement:

A thin flat plate is subjected to the following stresses: $\sigma$xx = 160 MPa; $\sigma$yy = 40 MPa; $\tau$xy = 80 MPa. Factor of safety is defined as the ratio of the yield stress to the applied stress. The yield stress of the material under uniaxial tensile load is 250 MPa. The factor of safety for the plate assuming that material failure is governed by the von Mises criterion is _____ (rounded off to two decimal places).
Question figure for GATE AE 2025 Q59

Scientific schematic diagram reproduced from official IIT paper

Official Answer Key:

1.25

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2025 Q.59)** **1. Intuitive Physical Setup & Given Parameters**: Plane stress state in a thin flat plate: - $\sigma_{xx} = 160\text{ MPa}$ - $\sigma_{yy} = 40\text{ MPa}$ - $\tau_{xy} = 80\text{ MPa}$ - Material uniaxial yield stress: $\sigma_y = 250\text{ MPa}$. We need to determine the Factor of Safety (FOS) using the **von Mises failure criterion** (rounded off to two decimal places). **2. Step-by-Step Failure Theory Derivation**: 1. **Von Mises Equivalent Stress ($\sigma_{\text{vm}}$) for Plane Stress**: \sigma_{\text{vm}} = \sqrt{\sigma_{xx}^2 - \sigma_{xx}\sigma_{yy} + \sigma_{yy}^2 + 3\tau_{xy}^2} 2. **Substitute Stress Components**: - $\sigma_{xx}^2 = 160^2 = 25600$ - $-\sigma_{xx}\sigma_{yy} = -(160)(40) = -6400$ - $\sigma_{yy}^2 = 40^2 = 1600$ - $3\tau_{xy}^2 = 3(80^2) = 3(6400) = 19200$ 3. **Sum Under the Radical**: \sigma_{\text{vm}}^2 = 25600 - 6400 + 1600 + 19200 = 40,000\text{ MPa}^2 \sigma_{\text{vm}} = \sqrt{40,000} = 200\text{ MPa} 4. **Compute Factor of Safety**: \text{FOS} = \frac{\sigma_y}{\sigma_{\text{vm}}} = \frac{250\text{ MPa}}{200\text{ MPa}} = 1.25 **3. Comprehensive Options & Distractor Analysis**: - **Evaluation Criteria**: Numerical Answer Type (NAT). - **Exact Analytical Result**: $\text{FOS} = 1.25$. - **Rounding Requirement**: Two decimal places $\implies \mathbf{1.25}$. **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **1.25** (Acceptable Range: **1.23 to 1.27**) - **Exam Takeaway**: In plane stress, $\sigma_{\text{vm}} = \sqrt{\sigma_x^2 - \sigma_x\sigma_y + \sigma_y^2 + 3\tau_{xy}^2}$. Here $\sqrt{25600 - 6400 + 1600 + 19200} = 200\text{ MPa}$, giving $\text{FOS} = 250/200 = 1.25$.
← Previous (Q58) All 2025 Questions Next (Q60) →

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