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AE GATE Exam Previous Papers 2016 | AE GATE Model Papers 2016
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GATE Aerospace Engineering Previous Paper 2016 Details
- Total number of Questions = 65
Few Question are listed below for preview: GATE Aerospace Engineering Previous Paper 2016
1. With increase in airfoil thickness, the critical Mach number for an airfoil is likely to
(A) decrease.
(B) increase.
(C) remain unchanged.
(D) be undefined
2. With increase in airfoil thickness, the critical Mach number for an airfoil is likely to
(A) decrease.
(B) increase.
(C) remain unchanged.
(D) be undefined
3. For a completely subsonic isentropic flow through a convergent nozzle, which of the following statement is TRUE?
(A) Pressure at the nozzle exit > back pressure.
(B) Pressure at the nozzle exit < back pressure.
(C) Pressure at the nozzle exit = back pressure.
(D) Pressure at the nozzle exit = total pressure
4. Which of the following aircraft engines has the highest propulsive efficiency at a cruising Mach number of less than 0.5?
(A) Turbofan engine
(B) Turbojet engine
(C) Turboprop engine
(D) Ramjet engine