Abstract
High frequency induction (electrodeless) plasmatrons provide the wide possibilities for modeling of nonequilibrium processes of dissociated gas flow thermochemical interaction with a surface at the conditions corresponding to hypersonic vehicle’s flight in atmosphere at high altitude [1].
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References
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© 1996 Kluwer Academic Publishers
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Vasil’Evskii, S.A., Kolesnikov, A.F., Yakushin, M.I. (1996). Mathematical Models for Plasma and Gas Flows in Induction Plasmatrons. In: Capitelli, M. (eds) Molecular Physics and Hypersonic Flows. NATO ASI Series, vol 482. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-0267-1_32
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DOI: https://doi.org/10.1007/978-94-009-0267-1_32
Publisher Name: Springer, Dordrecht
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