GATE AE 2025 • Q44 NAT • 2 Marks

Aerodynamics & Fluid Mechanics

Compressible Flow & Shocks

Subtopic: Rayleigh & Fanno Flow

Question Statement:

An approximate solution of the equation x3 - 17 = 0 is to be obtained using the Newton-Raphson method. If the initial guess is xo = 2 , the value at the end of the first iteration is x1 = _____ (rounded off to two decimal places).

Official Answer Key:

2.75

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2025 Q.44)** **1. Intuitive Physical Setup & Given Parameters**: We want to find an approximate solution to: $f(x) = x^3 - 17 = 0$ using the **Newton-Raphson method**. - Initial guess: $x_0 = 2$. We need to find the value $x_1$ at the end of the first iteration (rounded off to two decimal places). **2. Step-by-Step Mathematical Derivation**: 1. **Newton-Raphson Iteration Formula**: $x_{n+1} = x_n - \frac{f(x_n)}{f'(x_n)}$ 2. **Derivative of $f(x)$**: $f(x) = x^3 - 17 \implies f'(x) = 3x^2$ 3. **Evaluate at $x_0 = 2$**: $f(x_0) = 2^3 - 17 = 8 - 17 = -9$ $f'(x_0) = 3(2^2) = 3 \times 4 = 12$ 4. **Compute $x_1$**: $x_1 = 2 - \frac{-9}{12} = 2 + \frac{9}{12} = 2 + \frac{3}{4} = 2 + 0.75 = 2.75$ **3. Comprehensive Options & Distractor Analysis**: - **Evaluation Criteria**: Numerical Answer Type (NAT). - **Exact Analytical Result**: $x_1 = 2.75$. - **Rounding Requirement**: Two decimal places $\implies \mathbf{2.75}$. **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **2.75** (Acceptable Range: **2.73 to 2.77**) - **Exam Takeaway**: One step of Newton-Raphson: $x_1 = x_0 - \frac{x_0^3 - 17}{3x_0^2} = 2 - \frac{-9}{12} = 2.75$.

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