Numerical investigation of viscous chemically reacting gas flows near blunt-nosed bodies in the framework of Navier–Stokes equations
1Zabarko, DA, 1Kotenev, VP 1Open Joint Stock Company «Military Industrial Corporation« Scientific and Production Association of Mechanical Engineering», Reutov, Moscow region, Russia |
Kosm. nauka tehnol. 2005, 11 ;(Supplement1):036-042 |
https://doi.org/10.15407/knit2005.01s.036 |
Publication Language: Russian |
Abstract: Based upon the method of time-independent solution finding, a numerical method for integration of complete and parabolic Navie–Stokes equations is developed that allows one to compute hypersonic flows near blunt-nosed bodies taking into account nonequilibrium physical and chemical processes.
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1. Agafonov V. P., Vertushkin V. K., Gladkov A. A., Polyanskiy O. Yu. Non-equilibrium physico-chemical processes in aerodynamics. (Mashinostroenie, Moscow, 1972) [in Russian].
2. Vlasov V. I. The method of calculating the viscous shock layer, taking into account nonequilibrium physicochemical processes. Kosmonavtika i raketostroenie, No. 11, 5-12 (1997) [in Russian].
3. Kang S.-W. Nonequilibrium, ionized, hypersonic flow over a blunt body at low Reynolds number. Raketnaja tehnika i kosmonavtika, No. 7 (1970) [in Russian].
https://doi.org//10.2514/3.5883
4. Kokoshinskaya N. S., Pavlov B. M., and Paskonov V. M. Numerical Modeling of Supersonic Viscous Gas Flow Past Bodies. (Izd. MGU, Moscow, 1980) [in Russian].
5. Kotenev V. P., Sakharov V. I., Tirskii G. A. Calculation of supersonic spatial flow around blunted bodies, taking into account non-equilibrium chemical reactions. In: Issledovanija po giperzvukovoj ajerodinamike i teploobmenu s uchetom neravnovesnyh himicheskih reakcij. (Izd. MGU, Moscow, 1987) [in Russian].
6. Blottner F. G. Nonequilibrium Laminar Boundary Layer Flow of Ionized Air. Rept. R64SD56 (Space Sciences Laboratory, General Electric Co., Philadelphia, Pa., Nov. 1964).
https://doi.org//10.2514/6.1964-41
7. Rakich J. V., Bailey H. E., Park C. Computation of Nonequilibrium, Supersonic Three-Dimensional lnviscid Flow over Blunt-Nosed Bodies. AIAA J., 21 (6), 834- 841 (1983).
https://doi.org//10.2514/3.8160
8. Swaminathan S., Kim M. D., Lewis C. H. Nonequilibrium Viscous Shock-Layer Flows over Blunt Sphere-Cones at Angle of Attack. J. Spacecraft and Rockets, 20, July-August, 331-338 (1983).
https://doi.org//10.2514/3.25602