한국전산유체공학회:학술대회논문집

Korean Society of Computational Fluids Engineering (한국전산유체공학회)
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Study on Numerical Method for Combustion-Gas Flow Field of Granular Type Solid Propellant

과립형 고체추진제의 연소가스 유동장 해석을 위한 수치해석 기법 연구

  • 성형건 (인하대학교 대학원 항공공학과) ;
  • 장진성 (인하대학교 대학원 항공공학과) ;
  • 노태성 (인하대학교 항공우주공학과) ;
  • 최동환 (인하대학교 항공우주공학과)
  • Published : 2008.03.26
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Abstract

In this study, numerical methods for the code development of the interior ballistics have been conducted. Mathematical models and numerical methods for the analysis technique of the granular solid propellants have been investigated. As the results of applying the methods of errors have been generated by calculation for the specific surface area of the granular solid propellants. To remove these error, the developed Eulerian-Larangian method for multiphase flows has been suggested.

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