Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel
By: S. Venkateswaran, L. Roane Hunt, Ramadas K. Prabhu.
Contributors: Hunt, L. Roane; Prabhu, Ramadas K.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Series: NASA technical memorandum -- 4374.; NASA technical memorandum -- 4374.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; For sale by the National Technical Information Service]
Published: 1992
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Hypersonic wind tunnels -- Computer simulation.; Aerothermodynamics -- Computer simulation.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-2402-M.

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