한국전산유체공학회:학술대회논문집
- 2004.10a
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- Pages.155-160
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- 2004
Investigation on the shock-induced rocket separation from the mother plane
충격파에 의한 비정상 모선분리 현상 연구
Abstract
This paper describes a supersonic separation of air-launching rocket from the mother plane. Three dimensional Euler equations were numerically solved to analyze steady/unsteady state fluid flows. To solve the Euler equations, named CFD-FASTRAN that is commercial computation code. The results of simulation clearly demonstrate effect of shock-expansion wave interaction between the rocket and the mother plane. Moreover, important influential factors at separating stage of the rocket were extracted with a comprehensive analysis. Finally, from the consideration of supersonic-separation, a guideline to safety-separation is given to the design of supersonic air-launching rocket.
Keywords