Aerodynamic characteristics of a hypersonic research airplane concept having a 70ê swept double-delta wing at Mach number 0.2
By: Jim A. Penland, Theodore R. Creel, Jr., and James L. Dillion, Langley Research Center
Contributors: Creel, Theodore R., joint author; Dillon, James L., joint author; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical paper ; 1252
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: 78
Subjects: Hypersonic planes; Aerodynamics, Supersonic; Stability of airplanes; Lift (Aerodynamics)
Notes: Issued Sept. 1978

Includes bibliographical references