compressors gas turbines and jet engines MCQs – Page 8

Practise focused compressors gas turbines and jet engines questions with marked answers for exam preparation and subject revision.

compressors gas turbines and jet engines Mcqs
142. The working fluid in ai turbine is___________________?
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A. in three phases

B. in a single phase

C. in the form of air and water mixture

D. in two phases

E. gas and no air

143. The work ratio of a gas turbine plant is defined as the ratio of__________________?
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A. net work output and isentropic heat drop

B. net work output and heat supplied (6) net work output and work done by turbine

C. isentropic increase/drop in temperature and actual increase/ drop in temperature

D. actual heat drop and isentropic heat drop

145. An ideal air compressor cycle without clearance on p-v diagram can be represented by following processes________________?
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A. two isobaric, two adiabatic and one constant volume

B. one adiabatic, two isobaric, and one constant volume

C. two adiabatic, one isobaric and one constant volume

D. two adiabatic and two isobaric

E. one adiabatic, one isobaric and two constant volume

147. A centrifugal compressor works on the principle of__________________?
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A. combination of A. and D.

B. generating pressure directly

C. conversion of pressure energy into kinetic energy

D. conversion of kinetic energy into pressure energy

E. centripetal action

151. The compressor capacity with decrease in suction temperature_________________?
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A. remains unaffected

B. increases

C. increases upto certain limit and then decreases

D. decreases

E. may increase or decrease depending on compressor capacity

153. The volumetirc efficiency of a compressor is calculated on the basis of __________________?
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A. volume of air inhaled at N.T.P. conditions

B. volume of air inhaled at working conditions

C. none of the above

D. volume at 0C and 1 kg/cm2

E. volume at 20C and 1 kg/cm2

155. In the aircraft propellers __________________?
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A. all of the above

B. its functioning does not depend on presence of air

C. none of the above

D. propulsive matter is ejected from within the propelled body

E. the propulsive matter is caused to flow around the propelled body

156. For a compressor, least work will be done if the compression is________________ ?
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A. none of the above

B. somewhere in between isentropic and isothermal

C. isentropic

D. polytropic

E. isothermal
157. Fighter bombers use following type of engine __________________?
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A. ram-jet ,

B. turbo-propeller

C. pulsojet

D. turbo-jet

E. rocket

158. The advantage of multistage compression over single stage compression is ________________?
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A. all of the above

B. moisture free air

C. lower power consumption per unit of air delivered

D. decreased discharge temperature

E. higher volumetric efficiency

160. During base load operation, the best method of controlling compressor is ___________________?
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A. variable speed

B. relief valve

C. none of the above

D. start-stop motor

E. constant speed unloader