1. Which of the following statement is correct relating to rocket engines ?
2. A turbo-prop is preferred to turbo-jet because
3. The air power of the compressor is also known as
4. The minimum work required for a three stage reciprocating air compressor is __________ the work required for each stage
5. A rocket engine uses __________ for the combustion of its fuel
6. The ratio of the net work obtained from the gas turbine plant to the turbine work is known as
7. A jet engine has
8. The overall isothermal efficiency of the compressor is defined as the ratio of
9. In a high pressure compressor, the delivery pressure is
10. For minimum work required to compress and deliver a quantity of air by multi-stage compression,
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