Ram compression in turbojet involves Lost work Increasing speed of incoming air Compression of inlet air Reduction of speed of incoming air and conversion of part of it into pressure energy TRUE ANSWER : ? YOUR ANSWER : ?
Choose the correct statement Gas turbines has flat efficiency at part loads Gas turbine is capable of rapid start up and loading Gas turbines have high standby losses and require lot of maintenance Gas turbine requires lot of cooling water TRUE ANSWER : ? YOUR ANSWER : ?
A compressor at high altitudes will require ___ power. More Less Same None of the listed here TRUE ANSWER : ? YOUR ANSWER : ?
The air is delivered ________ in one revolution in case of a three lobbed rotor. Two times Six times Three times Four times TRUE ANSWER : ? YOUR ANSWER : ?
Intercooling in gas turbines Decreases net output but increases thermal efficiency Decreases net output and thermal efficiency both Increases net output and thermal efficiency both Increases net output but decreases thermal efficiency TRUE ANSWER : ? YOUR ANSWER : ?
The efficiency of jet engine is Lower at low speed Higher at high speed Same at all altitudes Higher at high altitudes TRUE ANSWER : ? YOUR ANSWER : ?
For a two stage reciprocating compressor, compression from p₁ to p₃ is with perfect intercooling and no pressure losses. If compression in both the cylinders follows the same polytropic process and the atmospheric pressure is pa, then the intermediate pressure p₂ is given by p₂ = Pa p₃/p₁ p₂ = p₁. p₃ p₂ = (p₁ + p₃)/2 P₂ = Pa × p₃/p₁ TRUE ANSWER : ? YOUR ANSWER : ?
The air power of the compressor is also known as Brake power None of these Indicated power Frictional power TRUE ANSWER : ? YOUR ANSWER : ?
The closed cycle in gas turbines In never used Provides greater flexibility Provides lesser flexibility Is used when gas is to be burnt TRUE ANSWER : ? YOUR ANSWER : ?
The type of rotary compressor used in gas turbines, is of Radial flow type None of the listed here Axial flow type Centrifugal type TRUE ANSWER : ? YOUR ANSWER : ?