131. The jnaximum combustion pressure in gas turbine as compared to I.C. engine is
Correct answer: (B)
less
132. The main purpose of reheating in gas turbine is to
Correct answer: (C)
increase power output
133. The material commonly used for air craft gas turbine is
Correct answer: (D)
Timken, Haste and Inconel allpys
134. The maximum compression ratio in an actual single stage axial flow comperssor is of the order of
Correct answer: (A)
01:01.2
135. The maximum propulsion efficiency of a turbojet is attained at around following speed –
Correct answer: (D)
2400km /hr
136. The- most efficient method of compressing air is to compress it
Correct answer: (A)
isothermally
137. The net work input required for compressor with increase in clearance volume
Correct answer: (C)
remains same
138. The overall isothermal eiffciency of compressor is defined as the ratio of
Correct answer: (A)
isothermal h.p. to the BHP of motor
139. The power available for take off and climb in case of turbojet engine as compared to reciprocating engine is
Correct answer: (A)
less
140. The pressure and temperature conditions of air at the suction of compressor are
Correct answer: (E)
pressure sightly less than atmospheric and temperature slightly more than atmospheric.