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Home⇒ Engineering⇒
Compressors gas turbine jet engine
1-Dont try to cram or spend more time here just read it fast and cover syllabus then practice MCQ's cheptor of same topic to check your progress. . |
2-Wrong options are also given but dont concentrate there, Right answer is in bold format. |
Q1 ⇒ For supplying intermittent small quantity of air at high pressure, following compressor is best suited reciprocating [other wrong options] [Discuss in forum] centrifugal axial screw turbo jet. |
Q2 ⇒ For minimum work in multistage compression, assuming same index of compression in all stages work done in all stages should be equal [other wrong options] [Discuss in forum] work done in first stage should be more work done in subsequent stages should increase work done in subsequent stages should decrease work done in any stage is no criterion for minimum work but depends on other factors. |
Q3 ⇒ For a two stage compressor* if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will increase [other wrong options] [Discuss in forum] decrease remain unaffected other factors control it unpredictable. |
Q4 ⇒ Diffuser in a compressor is used to convert kinetic energy into pressure energy [other wrong options] [Discuss in forum] increase velocity make the flow stream-line convert pressure energy into kinetic energy increase degree of reaction. |
Q5 ⇒ The ratio of isentropic work to euler's work is known as pressure coefficient [other wrong options] [Discuss in forum] compressor efficiency isentropic efficiency Euler's efficiency pressure ratio. |
Q6 ⇒ The thermodynamic efficiency of rotary compressor is based on adiabatic compression [other wrong options] [Discuss in forum] isothermal compression isentropic compression polytropic compression none of the above. |
Q7 ⇒ Phenomenon of choking in compressor means fixed mass flow rate regardless of pressure ratio [other wrong options] [Discuss in forum] no flow of air reducing mass flow rate with increase in pressure ratio increased inclination of chord with air steam does not occur. |
Q8 ⇒ The maximum compression ratio in an actual single stage axial flow compressor is of the order of 1 : 1.2 [other wrong options] [Discuss in forum] 1 : 2 1 : 5 1 : 10 1 : 1 |
Q9 ⇒ Maximum delivery pressure is a rotary air compressor is of the order of 10 kg/cm2 [other wrong options] [Discuss in forum] 6 kg/cm2 16 kg/cm2 25 kg/cm2 40 kg/cm2. |
Q10 ⇒ Surging is the phenomenon of unsteady, periodic and reversed flow [other wrong options] [Discuss in forum] air stream blocking the passage motion of air at sonic velocity air stream not able to follow the blade contour production of no air pressure. |
Q11 ⇒ The ratio of the increase in pressure in rotor blades to total increase in pressure in the stage is called degree of reaction [other wrong options] [Discuss in forum] pressure ratio pressure coefficient slip factor stage factor. |
Q12 ⇒ Axial flow compressor resembles turbine [other wrong options] [Discuss in forum] centrifugal pump reciprocating pump sliding vane compressor none of the above. |
Q13 ⇒ Axial flow compressor has the following advantage over centrifugal compressor larger air handling ability per unit frontal area [other wrong options] [Discuss in forum] higher pressure ratio per stage aerofoil blades are used higher average velocities none of the above. |
Q14 ⇒ Actual compression curve is in between isothermal and adiabatic [other wrong options] [Discuss in forum] same as isothermal same as adiabatic better than isothermal and adiabatic none of the above. |
Q15 ⇒ Atmospheric pressure is 1.03 kg/cm and vapor pressure is 0.03 kg/cm . The air pressure will be 1.00 kg/cm2 [other wrong options] [Discuss in forum] 1.03 kg/cm2 1.06 kg/cm2 0.53 kg/cm2 0.5 kg/cm2. |
Q16 ⇒ The pressure ratio of an ideal vaned compressor with increase in mass flow rate remains constant [other wrong options] [Discuss in forum] increases decreases first decreases and then increases unpredictable. |
Q17 ⇒ Rotary compressors are suitable for large discharge at low pressure [other wrong options] [Discuss in forum] large discharge at high pressure low discharge at high pressure low discharge at low pressure there is no such limitation. |
Q18 ⇒ The volumetric efficiency of compressor with increase in compression ratio will decrease [other wrong options] [Discuss in forum] increase remain same may increase/decrease depending on clearance volume none of the above. |
Q19 ⇒ Stalling of blades in axial flow compressor is the phenomenon of air stream not able to follow the blade contour [other wrong options] [Discuss in forum] air stream blocking the passage motion of air at sonic velocity unsteady periodic and reversed flow production of no air pressure. |
Q20 ⇒ Pick up the wrong statement axial flow compressors are bigger in diameter compared to centrifugal type [other wrong options] [Discuss in forum] centrifugal compressors deliver prac-tically constant pressure over a con-> siderable range of capacities Axial flow compressors have a sub-stantially constant delivery at variable pressures centrifugal compressors have a wider stable operating range than axial flow compressors axial flow compressors apt to be longer as compared to centrifugal type. |
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