JAA ATPL Test

SUBSONIC AERODYNAMICS

Basics, laws and definitions

Question	Correct	Score
1 of 63	0 of 0	0%

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 wing chord line and the direction of the relative wind/airflow.
	C)	the angle formed by the longitudinal axis of the aeroplane and the chord line of the wing.
	D)	the angle between the aeroplane climb path and the horizon..