Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31 ̊angle of attack and Mach 20 in helium
By: George C. Ashby, Jr., and Vernon T. Helms III
Contributors: Helms, V. T.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum ; NASA TM X-3560
Publisher: National Aeronautics and Space Administration
Published: 1977
Place of publication: [Washington]; Springfield, Virginia
Language: eng
Number of pages: 60
Subjects: Hypersonic wind tunnels.; Pressure -- Measurement.
Notes: Issued Oct. 1977.

Bibliography: p. 9.