Lifting-surface-theory results for thin elliptic wings of aspect ratio 3 with chordwise loadings corresponding to 0.5-chord plain flap and to parabolic-arc camber /

Lifting-surface-theory results for thin elliptic wings of aspect ratio 3 with chordwise loadings corresponding to 0.5-chord plain flap and to parabolic-arc camber / Stewart M. Crandall.

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Bibliographic Details
Main Author: Crandall, Stewart M.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Numerical analysis
Format: Government Document Book
Language:English
Published: Washington D.C. : National Advisory Committee for Aeronautics, 1946.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 1064.
Subjects:
Lift (Aerodynamics)
Airplanes > Wings.
Aspect ratio (Aerofoils)

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Call Number: Y 3.N 21/5:6/1064
Y 3.N 21/5:6/1064 Available Place a Hold

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