Analysis of the possibilities of local simulation of aerodynamic heating in a powerful VGU-3 HF-plasmatron
DOI10.1134/S0015462822601309OpenAlexW4310241385MaRDI QIDQ2107840
A. F. Kolesnikov, A. V. Chaplygin, S. L. Shchelokov, Sergey Galkin, S. A. Vasil'evskij
Publication date: 5 December 2022
Published in: Fluid Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1134/s0015462822601309
numerical solutionexperimental validationblunt bodydischarge channelatmosphere entry modelingenthalpy-stagnation pressure relationsubsonic high-enthalpy air flow
Experimental work for problems pertaining to fluid mechanics (76-05) General aerodynamics and subsonic flows (76G25) Reaction effects in flows (76V05) Ionized gas flow in electromagnetic fields; plasmic flow (76X05) Basic methods in fluid mechanics (76M99)
Cites Work
- Conditions of simulation of stagnation point heat transfer from a high- enthalpy flow
- Three-dimensional problem of radiative gasdynamics of the Apollo-4 command module during superorbital atmospheric entry
- Local modeling of the aerodynamic heating of the blunt body surface in subsonic high-enthalpy air flow. theory and experiment on a high-frequency plasmatron
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