Subsonic dynamic stability characteristics of two close-coupled canard-wing configurations / Richmond P. Boyden, Langley Research Center
Contributors: Langley Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical paper ; 1291
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: 76
Subjects: Vibration (Aeronautics) -- Damping; Stability of airplanes; Airplanes -- Wings, Canard
Notes: Oct. 1978

Includes bibliographical references