Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration
By: Blair B. Gloss, Langley Research Center
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical memorandum ; 78686
Publisher: National Aeronautics and Space Administration; Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 91
Subjects: Camber (Aerofoils); Airplanes -- Wings, Canard
Notes: July 1978

Includes bibliographical references