International Journal of Aeronautical and Space Sciences

  • 제17권1호
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  • Pages.1-7
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  • 2016
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  • 2093-274X(pISSN)
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  • 2093-2480(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
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Effects of Gas-surface Interaction Models on Spacecraft Aerodynamics

  • 투고 : 2015.01.08
  • 심사 : 2015.12.03
  • 발행 : 2016.03.30
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초록

The influence of boundary condition of the bodies with gas flows is one of the most important problems in high-altitude aerodynamics. In this paper presents the results of the calculation of aerodynamic characteristics of aerospace vehicle using Monte-Carlo method based on three different gas-surface interaction models - Maxwell model, Cercignani-Lampis-Lord (CLL) model and Lennard-Jones (LJ) potential. These models are very sensitive for force and moment coefficients of aerospace vehicle in the hypersonic free molecular flow. The models, method and results can be used for new generation aerospace vehicle design.

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참고문헌

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