A simplified mathematical model for calculating aerodynamic loading and downwash for midwing wing-fuselage combinations with wings of arbitrary plan form /
By Martin Zlotnick and Samuel W. Robinson, Jr.

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Main Author
Zlotnick, Martin.
Related Names
Robinson, Samuel W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.
Language(s)
English
Published
Washington, D.C. : National Advisory Committee for Aeronautics, 1953.
Subjects
Aerofoils.
Airplanes > Fuselage.
Airplanes > Wings.
Aerodynamic load > Mathematical models.
Note
"January 16, 1953."
Physical Description
36 p. : ill. ; 27 cm.
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