Isothermal

Isentropic

Adiabatic

Isochoric

**Euler's equation is applicable for****The minimum work required for a three stage reciprocating air compressor is ________ the work required…****Inter-cooling in multistage compressors is done****In a jet engine, the air-fuel ratio is****If p₁ is the pressure of air entering the L.P, cylinder and p₃ is the pressure of air…****Water gas is produced by****In a reciprocating air compressor, the compression work per kg of air****Turbofan engine employs****In the axial flow gas turbine, the work ratio is the ratio of****For minimum work required to compress and deliver a quantity of air by multistage compression****Which of the following statement is correct as regard to centrifugal compressors?****There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum.…****For a two stage reciprocating compressor, compression from p₁ to p₃ is with perfect intercooling…****The work ratio of a gas turbine plant is defined as the ratio of****Ratio of compression is the ratio of****Which of the following statement is correct?****The efficiency of roots blower ________ with the increase in pressure ratio.****Gas turbine as compared to steam turbine****Axial flow compressor has the following advantage over centrifugal compressor****Pick up the correct statement****If the flow of air through the compressor is perpendicular to its axis, then it is a****The degree of reaction in an axial flow compressor is defined as the ratio of static enthalpy rise in…****A machine used to raise the pressure of air is called****Which is false statement about advantages of multistage compressor in comparison to single stage compressor?****If p₁, is the pressure of air entering the L.P. cylinder and p₂ is the pressure of air…****The ratio of the discharge pressure to the inlet pressure of air is called****The mean effective pressure of the compressor is the****In a double acting compressor, the air is compressed****Propulsion efficiency of the following order is obtained in practice****The ideal efficiency of simple gas turbine cycle depends on**