Numerical Study of Comprehensive Kinetic Model in Plane Shock Wave Problem

The comprehensive kinetic model equation for unsteady one-dimensional flow is numerically solved to obtain a converging solution for a plane shock structure problem. This model equation is proposed by Oguchi on the basis of the Grad’s 13-moment approximation, and its collision term is expressed in a...

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Veröffentlicht in:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2003, Vol.51(596), pp.498-505
Hauptverfasser: Nagai, Ryoichi, Maeno, Kazuo, Honma, Hiroki
Format: Artikel
Sprache:eng ; jpn
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