ATPL - Airline Transport Pilot license - Principles of Flight Page 33

Questions Principles of Flight - ATPL Page 33

An aeroplane is flying through the transonic range. As the Mach Number increases the centre of pressure of the wing will move aft. This movement requires:	4 Answers
Which statement is correct about a normal shock wave ?	4 Answers
Mach buffet occurs:	4 Answers
The aft movement of the centre of pressure during acceleration through the transonic range will:	4 Answers
In case of supersonic flow retarded by a normal shock wave a high efficiency (low loss in total pressure) can be obtained if the Mach number in front of the shock is	4 Answers
An aeroplane, with a C.G. location behind the centre of pressure of the wing can only maintain a straight and level flight when the horizontal tail loading is:	4 Answers
How does positive camber of an aerofoil affect static longitudinal stability?	4 Answers
If an aeroplane exhibits insufficient stick force per g, this problem can be resolved by installing:	4 Answers
The effect on static stability of an aeroplane with a high wing as compared to a low wing is:	4 Answers
One method to compensate adverse yaw is:	4 Answers

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