The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Aircraft velocity)
(v₁² -v₂²)/2g
(v₁ - v₂)²/2g
(v₁² -v₂²)/g
(v₁ - v₂)²/g
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- Pick up the correct statement
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- Which of the following statement is correct?
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- Which of the following statement is correct?
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- The overall efficiency of the compressed air system is the
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- Choose the correct statement
- Maximum temperature in a gas turbine is of the order of