| Positive effect, because the centre of pressure shifts rearward at increasing angle of attack |
| No effect, because camber of the aerofoil produces a constant pitch down moment coefficient, independent of angle of attack |
| Positive effect, because the lift vector rotates backward at increasing angle of attack |
| Negative effect, because the lift vector rotates forward at increasing angle of attack |
MENU
EN 
IT
ES
DE
FR
PL
CZ
RS
Exam Questions
Training Quiz
Exam simulation
PDF Exam
Contact Us
Prices
Are you a school?
App Mobile