MENU
EN
IT
ES
DE
FR
PL
CZ
NL
HU
RS
EN 109 - ATPL - On an asymmetrical, single curve aerofoil, in subsonic airflow, at low angle of attack, when the angle of attack is increased, the centre of pressure will (assume a conventional transport aeroplane):
Question 109 - Principles of Flight - ATPL - Airline Transport Pilot license
This is 1 of over 400 exam questions on Principles of Flight
Take a test with 10 questions
