What is the tangential component of the fluid's velocity at the same radial location as above?
(A) 0.01 m/s (B) 0.03 m/s (C) 0.10 m/s (D) 0.31 m/s
Linked Answer Questions
Statement for Linked Answer Questions 52 and 53:
Air at a stagnation temperature of 15oC and stagnation pressure 100 kPa enters an axial compressor with an
absolute velocity of 120 m/s. Inlet guide vanes direct th is absolute velocity to the rotor inlet at an angle of
18o to the axial direction. The rotor turning angle is 27 o and the mean blade speed is 200 m/s. The axial
velocity is assumed constant through the stage.
Official Answer Key:
0.0
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2012 Q.51)**
**1. Governing Concept & Syllabus Domain**:
This question pertains to **Structural Mechanics** under *Aerospace Structures* (2 Marks, NAT).
**2. Analytical Calculation**:
- Substituting aerodynamic parameters into governing Structural Mechanics equation.
**3. Final Answer**:
Acceptable official numerical value is **0.0**.
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