The use of Richardson extrapolation in PNs solutions of rocket nozzle flow
Author:
Affiliation:
1. Physical Research, Inc., Irvine, CA
2. Software and Engineering Associates, Inc., Carson City, NV
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-2895
Reference44 articles.
1. Numerical Solution of Supersonic Viscous Flow over Blunt Delta Wings
2. 5 "AFWAL Parabolized Navier-Srokes Code: 1983 AFWAUNASA Merged Oawlinp Versions". US Air Force
3. Review of Problems in Application of Supersonic Combustion
4. A new technique for the numerical analysis of nonequilibrium flows
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Calculation of Numerical Uncertainty Using Richardson Extrapolation: Application to Some Simple Turbulent Flow Calculations;Journal of Fluids Engineering;1995-09-01
2. Performance and flow calculations for a gaseous H2/O2 thruster;Journal of Spacecraft and Rockets;1991-07
3. Numerical study of high-area-ratio H2/O2 rocket nozzles;27th Joint Propulsion Conference;1991-06-24
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