This page requires JavaScript. Please enable JavaScript in your browser and reload this page.
LIMITED PREVIEW |
Subscribe
|
Login
JAA ATPL Test
AviationTire.com | Oct-2024
081 PRINCIPLES OF FLIGHT - AEROPLANE
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 formed by the longitudinal axis of the aeroplane and the chord line of the wing.
B)
the angle for maximum lift/drag ratio.
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..