Other
Scientific paper
Feb 2005
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2005esasp.563..119s&link_type=abstract
Proceedings of the Fifth European Symposium on Aerothermodynamics for Space Vehicles (ESA SP-563). 8-11 November 2004, Cologne,
Other
Scientific paper
The thermally and chemically nonequilibrium flows in discharge channel of inductive plasmatron and in underexpanded air jets over a butt-end model are studied by CFD modeling. CFD modeling of entire flow field and heat transfer for supersonic high enthalpy air test conditions have been carried out for the 100-kW inductive plasmatron IPG-4 in the Institute for Problems in Mechanics Russian Academy of Science (IPM RAS) (Yakushin M., 1998). The results of the code-to-experiment validation in terms of the stagnation point heat transfer rates and stagnation pressure are reported. The differences in numerical results for various gas-phase models are analyzed.
Gromov V. V.
Sakharov V.
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