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Generalization of results of the computational modeling of streamline flow of a parachute by an undisturbed high-speed flow of gas using the method of large particles

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Abstract

On the basis of analysis of the numerical solution of the problem of aerodynamics of a parachute using the method of large particles, a simple analytical method of determining the pressure gradient on the canopy and the resistance coefficient of the parachute in a high-speed flow of gas is given. The results of computations coincide well with the experimental ones.

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Authors and Affiliations

  1. Moscow

    Yu. M. Davydov, Yu. V. Moseev, S. A. Logvinenko & T. V. Shukhova

Authors
  1. Yu. M. Davydov
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  2. Yu. V. Moseev
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  3. S. A. Logvinenko
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  4. T. V. Shukhova
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Additional information

Translated from Dinamicheskie Sistemy, No. 9, pp. 81–86, 1990.

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Davydov, Y.M., Moseev, Y.V., Logvinenko, S.A. et al. Generalization of results of the computational modeling of streamline flow of a parachute by an undisturbed high-speed flow of gas using the method of large particles. J Math Sci 70, 2014–2017 (1994). https://doi.org/10.1007/BF02110831

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  • DOI: https://doi.org/10.1007/BF02110831

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