Aerodynamic characteristics of a fixed arrow-wing supersonic cruise aircraft at Mach numbers of 2.30, 2.70, and 2.95
By: Odell A. Morris, Dennis E. Fuller, and Carolyn B. Watson, Langley Research Center
Contributors: Fuller, Dennis E., joint author; Watson, Carolyn B., joint author; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical memorandum ; 78706
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: 196
Subjects: Supersonic planes; Aerodynamics, Supersonic; Stability of airplanes; Lift (Aerodynamics)
Notes: Aug. 1978