The calculation of the pressure distribution over aerofoil sections of finite thickness with and without flaps and slabs

The calculation of the pressure distribution over aerofoil sections of finite thickness with and without flaps and slabs

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Bibliographic Details
Main Authors: 216570 Jacob, K., Riegels, Friedrich Wilhelm
Format:
Published: Farnborough, Hants : Ministry of Aviation, 1965
Subjects:
Aerodynamic load
Flaps (Airplanes)
Aerofoils

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