Calculation of aerodynamic loading and twist characteristics of a flexible wing at Mach numbers approaching 1.0 and comparison with experiment /
by John P. Mugler, Jr.

Description

Main Author

Mugler, John P.

Related Names

Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1960.

Subjects

Loads (Mechanics) > Loads (Mechanics) / Mathematical models.
Airplanes > Airplanes / Wings > Airplanes / Wings / Aerodynamics.

Physical Description

17 p. : ill. ; 26 cm.

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