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Is subsonic lifting surface theory relates to normal velocity?(a) True(b) FalseI have been asked this question in a national level competition.My question is based upon The Lifting Surface Theory topic in chapter Flow over Airfoils over Finite Wing of Aerodynamics

Answer»

Correct choice is (a) True

Best explanation: The BASIC integral equation of subsonic lifting surface THEORY relates the normal velocity distribution to the pressure difference distribution on a THIN wing and may be written in the FORM of the lifting surface theory.



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