Low-speed wind-tunnel study of the high-angle-of-attack stability and control characteristics of a cranked-arrow-wing fighter configuration
By: Sue B. Grafton
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical memorandum -- 85776
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1984
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 36
Subjects: Stability of airplanes -- Testing; Fighter planes -- Wings
Notes: "May 1984"--Cover

Distributed to depository libraries in microfiche

Subject category 08

Includes bibliographical references