Mechanical Engineering Exam > Mechanical Engineering Tests > Topicwise Question Bank for Mechanical Engineering > Test: Jet & Rocket Propulsion System - 2 - Mechanical Engineering MCQ
Test: Jet & Rocket Propulsion System - 2 - Mechanical Engineering MCQ
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10 Questions MCQ Test Topicwise Question Bank for Mechanical Engineering - Test: Jet & Rocket Propulsion System - 2
Test: Jet & Rocket Propulsion System - 2 for Mechanical Engineering 2024 is part of Topicwise Question Bank for Mechanical Engineering preparation. The Test: Jet & Rocket Propulsion System - 2 questions and answers have been
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Test: Jet & Rocket Propulsion System - 2 - Question 1
Propulsion efficiency is defined as the ratio of
Test: Jet & Rocket Propulsion System - 2 - Question 2
For maximum overall efficiency of a turbojet engine, the aircraft velocity and the jet velocity conform to the ratio
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Test: Jet & Rocket Propulsion System - 2 - Question 3
The thrust augmentation of turbojet engine can be effected by the following methods except
Test: Jet & Rocket Propulsion System - 2 - Question 4
The surrounding air is not used as oxidiser in
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Test: Jet & Rocket Propulsion System - 2 - Question 5
The propulsion system having highest efficiency at higher speed
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Test: Jet & Rocket Propulsion System - 2 - Question 6
Lowest thrust per unit engine weight is developed by
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Test: Jet & Rocket Propulsion System - 2 - Question 7
The power plant having highest specific fuel consumption
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Test: Jet & Rocket Propulsion System - 2 - Question 8
Which one of the following is the correct expression for the propulsion efficiency of a jet plane (neglecting the mass of fuel)?
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Test: Jet & Rocket Propulsion System - 2 - Question 9
The type of nozzle used in rocket propulsion system is
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