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Validation results for the LOGOS multifunction software package in solving problems of aerodynamics and gas dynamics for the lift-off and injection of launch vehicles

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Abstract

The paper discusses the applications of the LOGOS software package in the mathematical simulation of supersonic turbulent jets and transonic airfoil based on the Navier-Stokes equations with appropriate turbulence models. The calculation results are given for anisobaric flow streams. The theoretical and experimental results were compared for typical operation regimes of launch vehicle engines during lift-off. We give the results of the calculations for a transonic airfoil of a hammerhead payload fairing of a launch vehicle and compare them with the experimental data.

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Authors and Affiliations

  1. Central Machine Building Scientific and Research Institute (FSUE TsNIIMash), Korolev, Russia

    N. F. Kudimov, Yu. M. Lipnickiy, A. V. Panasenko & A. V. Safronov

  2. FSUE Russian Federal Nuclear Center—All-Russian Research Institute of Experimental Physics, Sarov, Russia

    Yu. N. Deryugin, R. N. Zhuchkov, D. K. Zelenskiy, A. S. Kozelkov & A. V. Sarazov

Authors
  1. Yu. N. Deryugin
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  2. R. N. Zhuchkov
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  3. D. K. Zelenskiy
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  4. A. S. Kozelkov
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  5. A. V. Sarazov
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  6. N. F. Kudimov
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  7. Yu. M. Lipnickiy
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  8. A. V. Panasenko
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  9. A. V. Safronov
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Corresponding author

Correspondence to A. V. Panasenko.

Additional information

Original Russian Text © Yu.N. Deryugin, R.N. Zhuchkov, D.K. Zelenskiy, A.S. Kozelkov, A.V. Sarazov, N.F. Kudimov, Yu.M. Lipnickiy, A.V. Panasenko, A.V. Safronov, 2014, published in Matematicheskoe Modelirovanie, 2014, Vol. 26, No. 8, pp. 83–95.

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Deryugin, Y.N., Zhuchkov, R.N., Zelenskiy, D.K. et al. Validation results for the LOGOS multifunction software package in solving problems of aerodynamics and gas dynamics for the lift-off and injection of launch vehicles. Math Models Comput Simul 7, 144–153 (2015). https://doi.org/10.1134/S2070048215020052

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