Comparison of nonequilibrium solution algorithms applied to chemically stiff hypersonic flows /

Bibliographic Details

Main Author:	Palmer, Grant
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Venkatapathy, Ethiraj
Format:	Government Document Book
Language:	English
Published:	Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration] ; [1995]
Series:	NASA technical memorandum ; 111955.
Subjects:	Algorithms. Descent trajectories. Hypersonic flow. Nonequilibrium flow. Robustness (Mathematics) Convergence. Blunt bodies. Reentry effects. Reentry vehicles.
Online Access:	https://purl.fdlp.gov/GPO/LPS54368