Experimental determination of effect of structural rigidity on rolling effectiveness of some straight and swept wings at Mach numbers from 0.7 to 1.7 /
by H. Kurt Strass, E. M. Fields, and Paul E. Purser.

Description

Main Author

Strass, H. Kurt.

Related Names

Purser, Paul E.
Fields, E. M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1950.

Subjects

Rolling (Aerodynamics)
Stability of airplanes, Lateral.
Airplanes > Airplanes / Wings, Swept-back.
Airplanes > Airplanes / Wings.

Note

"October 4, 1950."

Physical Description

40 p. : ill. ; 27 cm.

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