Catalog Record: Low-speed investigation of the effects of wing sweep on the aerodynamic characteristics of parawings having equal-length leading edges and keel | HathiTrust Digital Library

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Low-speed investigation of the effects of wing sweep on the aerodynamic characteristics of parawings having equal-length leading edges and keel /
by Rodger L. Naeseth and Thomas G. Gainer.

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Main Author: Naeseth, Rodger L.
Related Names: Gainer, Thomas G.
Language(s): English
Published: Washington [D.C.] : NASA, 1963.
Subjects: Wind tunnels.
Aerodynamics > Aerodynamics / Testing.
Airplanes > Airplanes / Parawings > Airplanes / Parawings / Aerodynamics > Airplanes / Parawings / Aerodynamics / Testing.
Note: "August 1963"--Cover.
"Langley Research Center Langley Station, Hampton, Va."--Cover.
"National Aeronautics and Space Administration."
"Technical Note D-1957."
Caption title.
This work is part of the library's "Parachute History Collection", donated by the Deutsches Zentrum für Luft- und Raumfahrt e.V. Institut für Flugsystemtechnik, through the American Institute of Aeronautics and Astronautics Aerodynamic Deceleration Systems Technical Committee.
Physical Description: [2], 78, [2] p. : ill. ; 28 cm.
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