A finite-step method for calculation of theoretical load distributions for arbitrary lifting-surface arrangements at subsonic speeds /
James A. Blackwell, Jr.

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Main Author
Blackwell, James A., Jr.
Related Names
Langley Research Center.
United States. National Aeronautics and Space Administration.
Language(s)
English
Published
Washington, D.C. : National Aeronautics and Space Administration ; 1969.
Subjects
Aerodynamics.
Airplanes > Wings > Aerodynamic load.
Aeronautics > Research.
Lift (Aerodynamics)
Load factor design.
Physical Description
40 p. : ill. ; 27 cm.
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