Aerodynamic characteristics of a hypersonic research airplane concept having a 70ê swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0
By: Jim A. Penland, James B. Hallissy
Contributors: Hallissy, James B; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical paper -- 1552
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, D.C; [Springfield, Va
Language: eng
Number of pages: 145
Subjects: Aerodynamics
Notes: "Langley Research Center."

"December 1979"--Cover

Includes bibliographical references