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#1. THE DRAG WHICH IS INVERSELY PROPORTIONAL TO SQUARE OF VELOCITY
#2. AILERON PROVIDE WHICH CONTROL
#3. IF AN AIRCRAFT HAVING INFINITE ASPECT RATIO THEN IT WILL NOT BE SUBJECTED TO
#4. THE AILERON CONTROL IS USED TO PROVIDE CONTROL AROUND
#5. IN STREAMLINE, THE AIR
#6. AT HIGH SPEED THE INDUCED DRAG
#7. IF THE ASPECT RATIO _________ , THE INDUCED DRAG WILL BE HALVED
#8. THE POINT AT WHICH LAMINAR FLOW IS CHANGED TO TURBULENT IS
#9. THE INCREASE OF ANGLE OF INCIDENCE FROM ROOT TO TIP
#10. THE ANGLE B/W CHORD LINE AND RELATIVE AIR FLOW IS
#11. THE STRAIGHT LINE WHICH GOES FROM LE OF THE WING TO THE TE IS CALLED
#12. THE LAYER OF AIR OVER THE SURFACE OF AN AIRFOIL WHICH IS SLOWER MOVING IN RELATION TO THE REST OF THE AIRFLOW IS KNOWN AS
#13. IF THE ASPECT RATIO IS HIGHER THAN INDUCED DRAG IS
#14. IF THE INDUCED DRAG IS REDUCED
#15. MTCS- HIGHER REYNOLDS NUMBER
#16. ON A DELTA WING AIRCRAFT LIFT
#17. INDUCED DRAG IS A PART OF
#18. THE DRAG IS CAUSED BY THE SEPARATION OF THE BOUNDARY LAYER
#19. NACA 0009 AIRFOIL IS HAVING
#20. FACTORS OF DRAG PRIMARILY DEPENDS ON