Design guide for pitch-up evaluation and investigation at high subsonic speeds of possible limitations due to wing-aspect-ratio variations /
by Kenneth P. Spreemann.

Description

Main Author

Spreemann, Kenneth P.

Related Names

United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington [D.C.] : National Aeronautics and Space Administration, [1959]

Subjects

Airplanes, Tailless.
Airplanes > Airplanes / Tail surfaces.
Aspect ratio (Aerofoils)
Pitching (Aerodynamics)
Airplanes > Airplanes / Wings > Airplanes / Wings / Design and construction.

Note

"August 1959."
Cover title.

Physical Description

37 p. : 15 ill. ; 27 cm.

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