81-01. Low Speed Aerodynamics
All questions: 645
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1. The point at which the resultant of lift forces acts is:
2. An aeroplane maintains straight and level flight while the speed is doubled. The change in lift coefficient will be:
3. Aslatis:
4. The increased upwash experienced at the leading edge of a wing when trailing edge flaps are lowered causes:
5. An aircraft whose weight is 237 402 N stalls at 132 kts. At a weight of 356 103 N it would stall at:
