Aerodynamic characteristics of a supersonic cruise airplane configuration at Mach numbers of 2.30, 2.96, and 3.30
By: Barrett L. Shrout and Roger H. Fournier, Langley Research Center
Contributors: Fournier, Roger H., joint author; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical memorandum ; 78792
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]; Springfield, Va
Language: eng
Number of pages: 141
Subjects: Supersonic planes; Stability of airplanes; Lift (Aerodynamics)
Notes: Jan. 1979

Includes bibliographical references