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ideal angle of attack
Definição1
The angle of attack of an aerofoil at which the air flows smoothly around the leading edge so as to produce a zero pressure differential across the leading edge. The ideal angle of attack depends only on the camber of the wing.
Fonte1
MULTILINGUAL aeronautical dictionary, or, dictionary aeronautique multilingue: english, french, spanish, dutch, greek, italian,portuguese, turkish. London, England: Technical Editing and reproduction Ltd, 1980. xx, 876 p. ISBN 92835016667
Subárea
Aerodynamics
Spanish
ángulo de ataque ideal