Analysis of Hypersonic Nozzles Including Vibrational Nonequilibrium and Intermolecular Force Effects
- 1 July 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (7) , 1243-1249
- https://doi.org/10.2514/3.49065
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Effects of vibrational nonequilibrium on axisymmetric hypersonic nozzle designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Assessment of flux vector splitting for viscous compressible flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- The solution of the Navier-Stokes equations using Gauss-Seidel line relaxationComputers & Fluids, 1989
- Current status of numerical solutions of the Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Systematics of Vibrational RelaxationThe Journal of Chemical Physics, 1963