Simulation of pressure and temperature responses for the 20 inch supersonic wind tunnel
By: Mark A. Motter.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 102647.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1990
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Computerized simulation.; Flow distribution.; Pressure effects.; Supersonic wind tunnels.; Temperature effects.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.