한국전산유체공학회:학술대회논문집
- 한국전산유체공학회 2001년도 춘계 학술대회논문집
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- Pages.144-148
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- 2001
로켓 노즐 유동의 열/화학적 특징 및 해석 기법
Thermochemcial Characteristics of Rocket Nozzle Flow and Methods of Analysis
초록
Characteristics of high temperature rocket nozzle flow is discussed along with the aspects of computational analysis. Three methods of nozzle flow analysis, frozen-equilibrium, shifting-equilibrium and non-equilibrium approaches, were discussed those were coupled with the methods of computational fluid dynamics. A chemical equilibrium code developed for the analysis of general hydrocarbon fuel was coupled with three approaches of nozzle flow analysis, and a test was made for a bell nozzle at typical operation condition. As a results, the characteristics of the approaches were discussed in aspects of rocket performance, thermal analysis and computational efficiency.
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