Low-speed wind-tunnel parametric investigation of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model
By: Delwin R. Croom
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical paper -- 1419
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1979
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 43
Subjects: Spoilers (Airplanes) -- Testing; Jet transports; Vortex-motion
Notes: "Langley Research Center."

Apr. 1979

Includes bibliographical references