한국추진공학회:학술대회논문집 (Proceedings of the Korean Society of Propulsion Engineers Conference)
- 한국추진공학회 2008년 영문 학술대회
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- Pages.659-665
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- 2008
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- 1975-342X(pISSN)
Numerical Study of Interior Ballistics with Moving Boundary
- Sung, Hyung-Gun (Department of Aerospace, Inha University) ;
- Park, Sol (Department of Aerospace, Inha University) ;
- Hong, Gi-Cheol (Department of Aerospace, Inha University) ;
- Roh, Tae-Seong (Department of Aerospace, Inha University) ;
- Choi, Dong-Whan (Department of Aerospace, Inha University)
- 발행 : 2008.03.30
초록
The 1-D numerical study of the interior ballistics has been conducted. The unsteady compressible 1-D CFD code using SIMPLER algorithm and QUICK scheme has been developed. The mathematical model of the two-phase flow has been established for the behavior of the interior ballistics. The moving boundary due to the projectile motion as the physical phenomena of the interior ballistics results in the varied control volume. In order to analyze the moving boundary, the numerical codes, which apply the ghost-cell extrapolation method and the Lagrangian method respectively, have been developed. The ghost-cell extrapolation method has been used in the Eulerian coordinate system. The Lagrangian method has been used in Non-Eulerian coordinate system. These codes have been verified through the analysis of the free piston motion problem in the tube. Through this study, the basic techniques of the numerical code for the multi-dimensional two-phase flow of the interior ballistics have been obtained.