Mathematical modeling of nitrogen flow around hypersonic bodies

Author:

Sidnyaev N. I.,Stolbova V. A.

Publisher

AIP Publishing

Reference22 articles.

1. Sidnyaev, N.I. (2004). Obzor metodik issledovaniya obtekaniya giperzvukovym potokom gaza tel s razrushayushchimsya pokrytiem [A review of methods for studying the flow around a body with a collapsing coating in a hypersonic gas flow]. Teplofizika i aeromekhanika [Thermophysics and Aeromechanics], 11 (4), 501–522.

2. Kolesnikov, A. F. (1993). Usloviya modelirovaniya v dozvukovyh techeniyah teploperedachi ot vysokoental’pijnogo potoka k kriticheskoj tochke zatuplennogo tela [Simulation conditions in subsonic heat transfer currents from a high-enthalpy flow to a critical point of a blunted body]. Izvestiya RAN. MZHG [Bulletin of the Russian Academy of Sciences. Fluid and gas mechanics], (1), 172–180.

3. Sidnyaev, N.I. (2005). Matematicheskoe modelirovanie himicheskogo aktivnogo pogranichnogo sloya pri diffuznom rezhime okisleniya [Mathematical modeling of the chemical active boundary layer in the diffuse mode of oxidation]. Moscow.: Izdatel’stvo MGTU [Moscow: Bauman press], 68–81.

4. Wenbo, M., Yin, Y., Nie, C., Dong, Y., Cheng, X., & Ai, B. (2017). Surface Recombination Effects on Aero-heating of High Enthalpy Flows. In 21st AIAA International Space Planes and Hypersonics Technologies Conference (p. 2196).

5. Dynamical Monte Carlo methods for plasma-surface reactions

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