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#1. THE THRUST OF GAS TUBINE ENGINE ________________
#2. THERMAL EFFICIENCY IS DEPENDS ON ________________________
#3. THE ABILITY OF AN ENGINE TO RUN SMOOTHLY AND GIVE DESIRED PERFORMANCE AT ALL SPEED FROM IDLING TO FULL POWER OUTPUT ?
#4. TO PREVENT SEIZURE OF CASE AND TURBINE
#5. TURBOJET ENGINE PRODUCE BY ______________
#6. TURBOSHAFT PREFERRED WHERE REQUIRED IS OF _______________
#7. CORROSIVE TYPE OF COMPOUND ARE WHICH TYPE OF PRODUCT ?
#8. PURPOSE OF EEC
#9. TYPE OF INLET DUCT USE IN GAS TURBINE ENGINE _______________
#10. THE BASIC PARAMETER FOR DESCRIBING THE FUEL ECONOMY OF THE AIRCRAFT ENGINE _____________
#11. VAPOUR LOCK IS DUE TO _____________
#12. IN TURBOPROP ENGINE CONSTANT RPM IS FUNCTION OF ____________
#13. THE THRUST OF ENGINE CALCULATED BY ____________
#14. WHICH TYPE FILTER USE JUST BEFORE OIL PASS FROM THE SPRAY NOZZLE ON TO THE BEARING SURFACE __________
#15. VAPOUR LOCK ?
#16. THE POWER PRODUCED BY A TURBINE ENGINE DEPENDS ON __________
#17. WHICH TYPE DUCT HAVE A BELL SHAPE FUNNEL HAVING CAREFULLY ROUNDED SHOULDER WHICH OFFER PRACTICALLY NO AIR RESISTANCE ?
#18. WHICH TYPE OF ENERGY EXTRACT BY TURBINE ?
#19. PRESSURE RELIEF VALVE SYSTEMS
#20. IN CAN TYPE COMBUSTION CHAMBER THE AIR ENTER THROUGH THE ____________
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