A gaseous mixture of air and fuel enters a constant area combustion chamber at a velocity of 100
m/s and at a static temperature of 300 K. The heat release due to combustion is 1000 kJ/kg. The
specific heat at constant pressure of the calorically perfect gas is 1000 J/kgK. The total temperature
of air-fuel mixture after combustion is ______ K.
Official Answer Key:
0.0
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2016 Q.33)**
**1. Governing Concept & Syllabus Domain**:
This question pertains to **Air-Breathing & Rocket Propulsion** under *Propulsion* (1 Mark, NAT).
**2. Analytical Calculation**:
- Substituting aerodynamic parameters into governing Air-Breathing & Rocket Propulsion equation.
**3. Final Answer**:
Acceptable official numerical value is **0.0**.
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