The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation 5% 0.5% 1.0% 0.1% TRUE ANSWER : ? YOUR ANSWER : ?
In a turbo jet engine, subsequent to heat addition to compressed air, to get the power output, the working substance is expanded in Turbine blades, which is essentially an isentropic process Turbine blades, which is a constant volume process Exit nozzle, which is a constant volume process Exit nozzle, which is essentially an isentropic process TRUE ANSWER : ? YOUR ANSWER : ?
The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Aircraft velocity) (v₁ - v₂)²/2g (v₁² -v₂²)/g (v₁² -v₂²)/2g (v₁ - v₂)²/g TRUE ANSWER : ? YOUR ANSWER : ?
For perfect intercooling in a three stage compressor p₁ p₂ = p₃ p₄ p₁ p₃ = p₂ p₄ p₂/p₁ = p₃/p₂ = p₄/p₃ p₃/p₁ = p₄/p₂ TRUE ANSWER : ? YOUR ANSWER : ?
Cylinder clearance in a compressor should be About 50% of swept volume As small as possible About 100% of swept volume As large as possible TRUE ANSWER : ? YOUR ANSWER : ?
The efficiency and work ratio of a gas turbine plant can be increased by All of these Adding heat exchanger Injecting water in/around combustion chamber Reheating the air after partial expansion in the turbine TRUE ANSWER : ? YOUR ANSWER : ?
The volume of air delivered in a medium capacity air compressor per unit time is 0.15 to 5 m³/s 0.1 to 1.2 m³/s Above 5 m³/s None of these TRUE ANSWER : ? YOUR ANSWER : ?
In a centrifugal compressor, the flow of air is ________ to the axis of compressor. Parallel Inclined Perpendicular None of these TRUE ANSWER : ? YOUR ANSWER : ?
Axial flow compressor has the following advantage over centrifugal compressor Aerofoil blades are used Higher average velocities Larger air handling ability per unit frontal area Higher pressure ratio per stage TRUE ANSWER : ? YOUR ANSWER : ?