GATE AE 2022 • Q14 MCQ • 1 Mark Aerodynamics & Fluid Mechanics

Aerodynamics & Fluid Mechanics

Compressible Flow & Shocks

Subtopic: Normal & Oblique Shock Waves

Question Statement:

The point of maximum entropy on a Fanno-curve in a Temperature-Entropy (T-s) diagram represents the
Question figure for GATE AE 2022 Q14

Scientific schematic diagram reproduced from official IIT paper

Options:

  • (A) maximum flow Mach number
  • (B) minimum flow Mach number
  • (C) sonic Mach number
  • (D) normal shock in the flow

Official Answer Key:

C

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2022 Q.14)** **1. Intuitive Physical Setup & Given Parameters**: We are asked to identify the physical state represented by the point of maximum entropy on a Fanno curve in a Temperature-Entropy ($T-s$) diagram. **2. Step-by-Step Mathematical Derivation**: 1. **Governing Equations of Fanno Flow**: Fanno flow describes 1-D steady, adiabatic flow of an ideal gas through a constant-area duct with wall friction. The governing conservation laws are: - Continuity: $\rho u = G = \text{const}$ - Energy: $h_0 = c_p T + \frac{u^2}{2} = \text{const}$ - Equation of State: $p = \rho R T$ 2. **Entropy Condition ($ds = 0$)**: Combining the Second Law $T ds = dh - v dp$ with the continuity and energy invariants yields: \frac{ds}{du} = \frac{u}{T} \left( \frac{u^2}{a^2} - 1 \right) = \frac{u}{T}(M^2 - 1) Setting $\frac{ds}{du} = 0$ for maximum entropy: M^2 - 1 = 0 \implies M = 1 3. **Physical Significance (Choking Limit)**: - The upper branch ($M < 1$) undergoes frictional heating and accelerates toward $M = 1$ with increasing entropy. - The lower branch ($M > 1$) undergoes frictional deceleration toward $M = 1$ with increasing entropy. - The maximum entropy point corresponds strictly to sonic flow ($M = 1$). Duct friction cannot drive flow past this point without changing inlet conditions (Fanno choking). **3. Comprehensive Options & Distractor Analysis**: - **(A) stagnation condition**: ❌ **INCORRECT**. Stagnation corresponds to $M = 0$ ($u = 0$, maximum temperature). - **(B) maximum pressure**: ❌ **INCORRECT**. Maximum pressure occurs at $M = 0$. - **(C) sonic condition (M = 1)**: ✅ **CORRECT**. At the point of maximum entropy on the Fanno curve, the local Mach number is strictly unity ($M = 1$). - **(D) maximum temperature**: ❌ **INCORRECT**. Maximum temperature occurs at $M = 0$ ($T = T_0$). **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **C** - **Exam Takeaway**: Both the Fanno curve (adiabatic with friction) and Rayleigh curve (frictionless with heat transfer) reach their maximum entropy points at exactly the sonic state $M = 1$.
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