mechanical-engineering-compressors-gas-dynamics-and-gas-turbines Related Question Answers

126. A simple turbo-jet engine is basically a gas turbine engine equipped with a propulsive nozzle and diffuser.



127. If the flow of air through the compressor is parallel to its axis, then the compressor is





128. The volumetric efficiency of the compressor is defined as the ratio of volume of free air delivery per stroke to the swept volume of the piston.



129. A centrifugal compressor is an axial flow compressor.



130. A compressor must be driven by some prime mover.



131. The gas used in fire extinguishers is:?





132. Volumetric efficiency of a compressor decreases with __________ in compression ratio.



133. The overall thermal efficiency of an ideal gas turbine plant is (where r = Pressure ratio)



134. The speed of rotary air compressor is __________ as compared to reciprocating air compressor.



135. When air is to be compressed at a high pressure, then it is advantageous to use





136. The absolute pressure of air at the outlet of a compressor is called





137. The degree of reaction is usually kept __________ for all types of axial flow compressors.





138. Standard air is the air at __________ and relative humidity of 36 percent.





139. In a single stage, single acting reciprocating air compressor without clearance volume, the workdone is maximum during





140. The compressor capacity is defined as the





141. The Stone Age people had the first domestic?





142. The operation of the reciprocating air motor is similar to reciprocating air compressor.



143. The volume of air sucked by the compressor during its suction stroke is called





144. For perfect intercooling in a two stage compressor,



145. ‘Arrears’ best means :?





146. The volumetric efficiency of a compressor





147. Reheating in a multi-stage expansion gas turbine __________ compressor work.




148. The multi-stage compression ofair as compared to single stage compression





149. Which one of the following is the effect of blade shape on performance of a centrifugal compressor ?





150. In a jet engine, the air-fuel ratio is





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