Compressors, Gas Dynamics and Gas Turbines - Data Intensity 2 Multiple Questions and Answers.
Exercise Questions ::
Compressors, Gas Dynamics and Gas Turbines
21. | Only rocket engines can be propelled to space because |
| |
| A. | they can generate very high thrust |
| B. | they have high propulsion efficiency |
| C. | these engines can work on several fuels |
| D. | they are not air-breathing engines |
|
|
Published by:Michael Daani
Published by:Michael Daani
23. | High air-fuel ratio in gas turbines |
| |
| A. | increases power output |
| B. | improves thermal efficiency |
| C. | reduces exhaust temperature |
| D. | do not damage turbine blades |
|
|
Published by:Michael Daani
24. | The ratio of the volume of free air delivery per stroke to the swept volume of the piston, is known as |
| |
| A. | compressor efficiency |
| B. | volumetric efficiency |
| C. | isothermal efficiency |
| D. | mechanical efficiency |
|
|
Published by:Michael Daani
25. | The ratio of the indicated power to the shaft power or brake power of the motor or engine required to drive the compressor, is called |
| |
| A. | compressor efficiency |
| B. | volumetric efficiency |
| C. | isothermal efficiency |
| D. | mechanical efficiency |
|
|
Published by:Michael Daani
«»