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AERODYNAMIC CHARACTERISTICS OF AN AIRCRAFT WITH A COMPLEX SHAPE TAKING INTO ACCOUNT THE POTENTIAL OF MOLECULAR FLOWINTERACTION WITH A SURFACE

Volumen 41, Ausgabe 5, 2010, pp. 551-566
DOI: 10.1615/TsAGISciJ.v41.i5.50
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ABSTRAKT

The investigation of the influence of boundary conditions of bodies in a flow is one of the most important problems in aerodynamics. This problem is especially important when aircraft move at a high altitude, i.e., at the regimes described by the molecular distribution function. This is an orbital flight of space vehicles, and a motion of aerospace systems in the upper atmosphere. Models of flows of molecules with different potentials of interaction are proposed in this paper. The boundary conditions are approximated on a wide range of regimes. The results of the calculation of aerodynamic characteristics of an airspace vehicle in the transitional regime are presented.

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REFERENZIERT VON
  1. Ivanovich Khlopkov Yuri, Myint Zay Yar Myo, Yurievich Khlopkov Anton, Aerodynamic Investigation for Prospective Aerospace Vehicle in the Transitional Regime, International Journal of Aeronautical and Space Sciences, 14, 3, 2013. Crossref

  2. Khlopkov Yuri Ivanovich, Chernyshev Sergey Leonidovich, Myint Zay Yar Myo, Khlopkov Anton Yurievich, Effects of Gas-surface Interaction Models on Spacecraft Aerodynamics, International Journal of Aeronautical and Space Sciences, 17, 1, 2016. Crossref

  3. Khlopkov Yuri Ivanovich, Khlopkov Anton Yurievich, Myint Zay Yar Myo, Computer Modelling of Aerothermodynamic Characteristics for Hypersonic Vehicles, Journal of Applied Mathematics and Physics, 02, 05, 2014. Crossref

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