The ratio of specific weighf/h.p. of gas turbin and I.C engines may be typically of the order of_______________________?

Related Mcqs:

Adiabatic compression is one in which___________________?

A. temperature during compression remains constant B. no heat leaves or enters the compressor cylinder during cornpression C. temperature rise follows a linear relationship D. work done is maximum E. entropy decreases...

For a two stage compressor* if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will___________________?

A. increase B. decrease C. remain unaffected D. other factors control it E. unpredictable...

The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio_____________________?

A. increases B. decreases C. first increases and then decreases D. first decreases and then increases E. remains same...

A rocket engine for the combustion of its fuel_____________________?

A. carries its own oxygen B. uses surrounding air C. uses compressed atmospheric air D. does not require oxygen E. depends on electrical energy supplied by solar cells...

The working fluid in ai turbine is___________________?

A. in two phases B. in three phases C. in a single phase D. in the form of air and water mixture E. gas and no air...