A.unequal
B.equal
C.not related to each other
D.none of the above
Related Mcqs:
- A gas turbine cycle operates through pressures ratio of 5. Air enters the compressor at atmospheric pressure and 25?C and entry to the turbine is at 800?C. The thermal efficiency of the plant has been found to be 37%. Now, if compressor and turbine efficiencies of 80% are taken into account, the value, of thermal efficiency will be
- A gas turbine plant operates between 1 ata and 9 ata with minimum and maximum cycle temperature of 25?C and 1000?C. A two stage compressor is provided with perfect intercooling and work is equally divided between the two stages. The intermediate pressure will be
- The compressor used in gas turbine is usually
- Overall efficiency of a gas turbine is
- The work done on a compressor will be least when air is taken from
- Shear stresses on mutually perpendicular planes are
- For minimum work in multistage compression, the work done on
- In a jet propulsion unit the products of combustion after passing through the gas turbine are discharged into
- Which of the following is a false stagement: The cause of excessive engine vibrations especially at high speeds in spark ignition engines is
- In a hydroelectric plant a conduit-system for taking water from the intake work to the turbine is known as