Theoretical lift due to wing incidence of slender wing-body-tail combinations at zero angle of attack / Alvin H. Sacks.

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Bibliographic Details
Main Author:	Sacks, Alvin H.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1956.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 3796.
Subjects:	Cylinders > Aerodynamics. Airplanes > Wings. Airplanes > Tail surfaces. Aerofoils. Angle of attack (Aerodynamics) Lift (Aerodynamics)

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Call Number:	Y 3.N 21/5:6/3796
Y 3.N 21/5:6/3796	Available Place a Hold