Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 /

Bibliographic Details

Main Author:	Shrout, Barrett L.
Corporate Authors:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Langley Research Center
Other Authors:	Corlett, William A., Collins, Ida K.
Format:	Government Document Book
Language:	English
Published:	Greeenbelt, Md. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; 1979.
Series:	NASA technical memorandum ; 80061.
Subjects:	Aerodynamics, Supersonic.