GATE AE 2007 • Q13 MCQ • 1 Mark Aerodynamics & Fluid Mechanics

Aerodynamics & Fluid Mechanics

Compressible Flow & Shocks

Subtopic: Normal & Oblique Shock Waves

Question Statement:

Across a normal shock

Options:

  • (A) both total temperature and total pressure decrease
  • (B) both total temperature and total pressure remain constant
  • (C) total pressure remains constant but total temperature decreases
  • (D) total temperature remains constant but total pressure decreases

Official Answer Key:

D

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2007 Q.13)** **1. Normal Shock Governing Relations**: Across a normal shock wave in a calorifically perfect gas: - **Total Temperature ($T_0$)**: Because the shock is an adiabatic process with no work or heat transfer ($\dot{q} = 0, \dot{w} = 0$), the total enthalpy and therefore total temperature remain strictly constant: $$T_{02} = T_{01}$$ - **Total Pressure ($P_0$)**: The normal shock involves severe internal dissipation and entropy generation ($\Delta s > 0$). By the thermodynamic $T\,ds$ relation: $$\frac{P_{02}}{P_{01}} = e^{-\Delta s / R} < 1$$ Thus, total pressure decreases across the shock wave. **2. Official Master Key**: - **Official Answer Key**: **D** (total temperature remains constant but total pressure decreases) - **Exam Takeaway**: Shock waves are adiabatic ($T_0 = \text{const}$) but irreversible (entropy increases, causing a loss in total pressure $P_0$).
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