Real gas flow parameters for NASA Langley 22-inch Mach 20 helium tunnel
By: Brian R. Hollis.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Series: NASA contractor report -- 4462.; NASA contractor report -- NASA CR-4462.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; National Technical Information Service, distributor]
Published: 1992
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Gases, Real.; Hypersonic wind tunnels.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 93-0029-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1992. 1 microfiche.