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Home > Exam Questions > ATPL - Airline Transport Pilot Licence > Principles of Flight > For a conventional aerofoil at unchanged dynamic pressure, increasing angle of attack just beyond the angle of CLmax into the stall normally causes lift (1) and drag (2), compared with the values at CLmax, to:

115 - ATPL Question Bank in English - For a conventional aerofoil at unchanged dynamic pressure, increasing angle of attack just beyond the angle of CLmax into the stall normally causes lift (1) and drag (2), compared with the values at CLmax, to:

Question 115 - Principles of Flight - ATPL - Airline Transport Pilot Licence

(1) decreases (2) decreases

(1) increases (2) increases

(1) decreases (2) increases

(1) increases (2) decreases

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