ATPL: The lift of an aeroplane of weight W in a constant linear climb with a climb angle (gamma) is approximately:
Domanda 24, Principles of Flight - ATPL - Airline Transport Pilot license
| W (1-tan.gamma) |
| W (1-sin.gamma) |
| W / cos.gamma |
| W cos.gamma |
| W (1-tan.gamma) |
| W (1-sin.gamma) |
| W / cos.gamma |
| W cos.gamma |
