ATPL: The lift coefficient (CL) of an aeroplane in steady horizontal flight is 0.35. An increase in angle of attack of 1 degree would increase CL by 0.079. If a vertical gust instantly changes the angle of attack by 2 degrees, the load factor will be:

Home > Archivio Quiz di Esame > Quiz ATPL - Test di esame Airline Transport Pilot license > Principles of Flight > The lift coefficient (CL) of an aeroplane in steady horizontal flight is 0.35. An increase in angle of attack of 1 degree would increase CL by 0.079. If a vertical gust instantly changes the angle of attack by 2 degrees, the load factor will be:

Domanda 301, Principles of Flight - ATPL - Airline Transport Pilot license

0.9

1.45

1.9

0.45

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