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Solution of internal problems of aerodynamics under transitional conditions using a model kinetic equation

  • A. I. Ivanovskii
  • S. Kh. Rozenfel'd
Article
  • 20 Downloads

Abstract

A method is developed based on the use of a model kinetic equation with a shock frequency ω = v/l (l is the mean length of the free flight path; v is the modulus of the molecular velocity). The method is tested on several classical problems.

Keywords

Mathematical Modeling Mechanical Engineer Industrial Mathematic Kinetic Equation Classical Problem 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Literature cited

  1. 1.
    D. G. M. Anderson, H. Baum, and M. Krook, “The current status of statistical models in kinetic theory,” in: Rarefied Gas Dynamics, Vol. 1, Acad. Press, New York-London (1969).Google Scholar
  2. 2.
    M. N. Kogan, The Dynamics of a Rarefied Gas [in Russian], Izd. Nauka, moscow (1967).Google Scholar
  3. 3.
    C. Cercignani, “Plane Poiseuille flow and Knudsen minimum effect,” in: Rarefied Gas Dynamics, Vol. 2, Academic Press (1963).Google Scholar
  4. 4.
    B. T. Porodnov, P. E. Suetin, and S. F. Borisov, “The flow of gases in a flat slit over a wide range of Knudsen numbers,” Zh. Tekh. Fiz.,40, No. 11 (1970).Google Scholar

Copyright information

© Consultants Bureau 1974

Authors and Affiliations

  • A. I. Ivanovskii
    • 1
  • S. Kh. Rozenfel'd
    • 1
  1. 1.Moscow

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