ATPL: How does positive camber of an aerofoil affect static longitudinal stability?
Domanda 327, Principles of Flight - ATPL - Airline Transport Pilot license
| 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 |
