Journal of Industrial Technology (산업기술연구)
- Volume 20 Issue B
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- Pages.45-53
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- 2000
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- 1229-9588(pISSN)
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- 1598-1371(eISSN)
The Variation of Thrust Distribution of the Rocket Nozzle Exit Plane with the Various Position of Secondary Injection
2차 분사의 위치 변화에 따른 로켓노즐 출구에서의 추력 분포 변화
- Published : 2000.12.31
Abstract
A numerical study is done on the thrust vector control using gaseous secondary injection in the rocket nozzle. A commercial code, PHOENICS, is used to simulate the rocket nozzle flow. A