ATPL: The lift coefficient (CL) of an aeroplane in steady horizontal flight is 0.42. An increase in angle of attack of 1 degree increases CL by 0.1. A vertical up gust instantly changes the angle of attack by 3 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 0.42. An increase in angle of attack of 1 degree increases CL by 0.1. A vertical up gust instantly changes the angle of attack by 3 degrees. The load factor will be:

Domanda 20, Principles of Flight - ATPL - Airline Transport Pilot license

0.74

1.71

2.49

1.49

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