Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30
By: Barrett L. Shrout, William A. Corlett, and Ida K. Collins
Contributors: Corlett, William A; Collins, Ida K; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical memorandum -- 80061
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1979
Place of publication: Greeenbelt, Md; [Springfield, Va
Language: eng
Number of pages: 55
Subjects: Aerodynamics, Supersonic
Notes: "Langley Research Center."

"May 1979"--Cover

Subject category 02

Includes bibliographical references