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JAA ATPL Test

AviationTire.com | Nov-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 formed by the longitudinal axis of the aeroplane and the chord line of the wing.

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

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