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JAA ATPL Test

AviationTire.com | Sep-2018

081 PRINCIPLES OF FLIGHT - AEROPLANE


SUBSONIC AERODYNAMICS
Basics, laws and definitions

QuestionCorrectScore
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The term angle of attack in a two dimensional flow is defined as:

A)the angle for maximum lift/drag ratio.

B)the angle between the aeroplane climb path and the horizon..

C)the angle between the wing chord line and the direction of the relative wind/airflow.

D)the angle formed by the longitudinal axis of the aeroplane and the chord line of the wing.