Numerical Simulation of Shock Wave in a Vortex Dominant Flow
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概要
- 論文の詳細を見る
In order to understand shock wave in a vortex dominant flow, we have presented simulation and visualization of supersonic impinging jet flows. We applied the MUSCL TVD scheme to convection terms and 2nd-order centered difference scheme for viscosity terms. And we used Cartesian coordinate system at equal intervals. Cartesian grids make grid generation time short and the process simple. By numerical results, we showed clearly image of a supersonic impinging jet and interaction of shock wave and vortex.
- 一般社団法人日本機械学会の論文
- 2004-09-04
著者
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Kawamura Tetuya
Graduate School of Humanities and Sciences, Ochanomizu University
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Kuwahara Kunio
The Institute of Space and Astronautical Science
-
Lee Mi
Ochanomizu University
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KAWAMURA Tetuya
Ochanomizu University
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Kawamura Tetuya
Ochanomizu Univ.
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