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): | ATPL | ID: 109

Home > Examination quizzes for PPL(A), PPL(H), BPL Gas, BPL Hot Air, ATPL, SPL - Sailplane, EASA Drone > Quiz ATPL - Exam test Airline Transport Pilot license > Principles of Flight > 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 id 109 - Principles of Flight - ATPL - Airline Transport Pilot license

Move aft

Remain matching the airfoil aerodynamic centre

Move forward

Remain unaffected

Training! Question explanation