Reacting multi-species gas capability for USM3D flow solver /

Bibliographic Details

Main Author:	Frink, Neal T.
Corporate Authors:	NASA Engineering and Safety Center, Langley Research Center
Other Authors:	Schuster, D. M. (David M.)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
Series:	NASA technical memorandum ; 2012-217575.
Subjects:	Navier-Stokes equation. Safety. Launch vehicles. Gas flow. High temperature gases. Temperature effects. Jet impingement. Ares 1 launch vehicle.
Online Access:	https://purl.fdlp.gov/GPO/gpo28375