Module 8 Set 3

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Results

#1. AT STALLING ANGLE, THE C OF P

#2. AT HIGHER ALTITUDE, TAS

#3. IN CLIMBING TURN, ROLLING ________

#4. ________ INCREASES, INDUCED DRAG DECREASES

#5. WHICH OF THE FOLLOWING PROPERTY AFFECTS THE AIRCRAFT PERFORMANCE?

#6. PITCHING ONLY IS CONTROLLED BY _______

#7. WHICH OF THE FOLLOWING IS AUTOMATICALLY ACTIVATED WHEN CONTROL IS FAILED ?

#8. WHEN LIFT GENERATED THEN __________ IS PRODUCED.

#9. WHICH OF THE FOLLOWING IS CONTRIBUTED IN LONGITUDINAL STABILITY ?

#10. STICK FIXED MEANS ________________________

#11. IF THE NOSE OF THE PLANE IS DOWN, THEN GLIDING IS ________

#12. COEFFICIENT OF VISCOSITY IS___________

#13. WHICH OF THE FOLLOWING STABILITY IS VERY DIFFICULT FOR ACHIEVING ?

#14. WHEN THE AIRCRAFT MOVE FORWARD DISTANCE IN UNIT WEIGHT OF FUEL THEN

#15. APPLICABLE NEWTONS LAWS OF AIR

#16. IN STRAIGHT AND LEVEL FLIGHT _____

#17. AS THE ALTITUDE INCREASES, COEFFICIENT OF VISCOSITY _______

#18. SWEEP BACK ANGLE EFFECTS

#19. IN DELTA WING A/C, LIFT ______

#20. LONGITUDINAL STABILITY IS DUE TO

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