Breakdown of continuum solvers in rapidly expanding flows

Author:

Gilmore Martin,Gallis Michael,Harvey John

Publisher

American Institute of Aeronautics and Astronautics

Reference3 articles.

1. Macrossan, M N 'Diatomic Collision Models used intheMonte-Carlodirect simulation methodapplied toRarefied Hypersonic flow,'Ph.D Thesis,Univ. of London,1983. "Gihore, M.R 'Comparison of Numerical Methods 1: DSMC simulations'and NS Predictions on Bluff Bodies,' 19thISSW,MarseillesFrance, 1993. "Gilmore, M R and Warburton, K 'Axi-Symmetric Hypersonic Jet Interaction : A combined Experimental and Computational Study. AIAA 95-0414.1995. I,Gallis, M and HNvey, J.K 'Comparison of the Maximum Entropy DSMC code with Flow Field Measurements,' AIAA95-0413,1995 "Van Wylen, G.A and Sonntag,R.E. Fundamenrals of Classical Thermodynamics,J Wiley & Sons, 1985. "Liepmann and Roshko,EIemenrsof GasDynamics, 3Wiley &Sons, 1957. '6Muntz,E P. 'The Electron Be'm Fluorescence Technique,' AGARDograph 132,1968. 17Kreyszig, G, Advanced Engineering Marhemarics.

2. investigation of low-density supersonic jets of hydrogen,'JFluid Mech., pp 41,Vol 280, 1994.

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