Application of finite difference TVD methods in hypersonic aerodynamics. The numerical method for solving of the hypersonic nonequilibrium aerogasdynamics problems is suggested. The method is based on the full three-dimensional Navier-Stokes equations, supplemented by the equations of chemical kinetics and the finite difference TVD method. The developed algorithms are implemented in the computer-aided software package SIGMA. The results of simulation of the hypersonic flow about the spherical nose segment of a model hypersonic vehicle are presented.
Keywords for this software
References in zbMATH (referenced in 4 articles , 1 standard article )
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- Dimitrienko, Yu. I.; Dimitrienko, I. D.: Modeling and simulation of textile composite plates under a punching load (2020)
- Kuzenov, Viktor V.; Shumaev, Vyacheslav V.: Estimation of instabilities under the joint action of laser radiation and a magnetic field on a plasma (2020)
- Dimitrienko, Yury; Koryakov, Mikhail; Zakharov, Andrey: Numerical modeling of coupled problems of external aerothermodynamics and internal heat-and-mass transfer in high-speed vehicle composite constructions (2017)
- Dimitrienko, Yury; Koryakov, Mikhail; Zakharov, Andrey: Application of finite difference TVD methods in hypersonic aerodynamics (2015)