Surface pressure data on a series of analytic forebodies at Mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip
By: James C. Townsend ... [et al.].
Contributors: Townsend, James C. 1938-; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.; Langley Research Center.
Series: NASA technical memorandum -- 80062.
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: 307
Subjects: Unsteady flow (Aerodynamics); Wind tunnels -- Flow visualization.; Aerodynamics, Supersonic.
Notes: "Langley Research Center."

"June 1979"--Cover.

Chiefly tables.

Includes bibliographical references.