A. turbo-jet engine
B. ram-jet engine
C. propellers
D. rockets
E. hydraulic jet propulsion
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Related Mcqs:
- Isothermal compression efficiency, even when running at high speed, can be approached by using A. multi-stage compression B. cold water spray C. both A. and B. above D. fully insulating the cylinder E. high stroke_________________?
- Isothermal compression efficiency, even when running at high speed, can be approached by using A. multi-stage compression B. cold water spray C. both A. and B. above D. fully insulating the cylinder E. high stroke...
- For slow-speed large capacity compressor, following type of valve will be best suited________________?
- A. poppet valve B. mechanical valve of the corliss, sleeve, rotary or semirotary type C. disc or feather type D. any of the above E. none of the above...
- The maximum propulsion efficiency of a turbojet is attained at around following speed __________________?
- A. 550 km/hr B. 1050km/hr C. 1700 km/hr D. 2400km /hr E. 4000 km/hr...
- Isothermal compression effeicency can be attained by running the compressor__________________?
- A. at very high speed B. at very slow speed C. at average speed D. at zero speed E. isothermally...
- What will be the volume of air at 327°C if its volume at 27°C is 1.5 m3/mt ?
- A. 3 m3/mt B. 1.5 m3/mt C. 18 m3/mt D. 6 m3/mt E. 0.75 m3/mt...
- Euler’s equation is applicable for__________________?
- A. centrifugal compressor B. axial compressor C. pumps D. all of the above E. none of the above...
- During peak load periods, the best method of controlling compressors is___________________?
- A. start-stop motor B. constant speed unloader C. relief valve D. variable speed E. none of the above...
- As the value of index ‘«’ is decreased, the volumetric efficiency will___________________?
- A. increase B. decrease C. remain unaffected D. may increase/decrease depending on compressor clearance E. none of the above...
- Rotary compressors are suitable for ____________________?
- A. large discharge at high pressure B. low discharge at high pressure C. large discharge at low pressure D. low discharge at low pressure E. there is no such limitation...
- High air-fuel ratio is used in gas turbines______________________?
- A. to increase the output B. to increase the efficiency C. to save fuel D. to reduce the exit temperature E. none of the above...
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