한국연소학회:학술대회논문집
- 한국연소학회 2007년도 제34회 KOSCO SYMPOSIUM 논문집
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- Pages.79-85
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- 2007
수직 연료 분사기구를 포함하는 HyShot 스크램제트 연소기의 동적 연소 유동해석
Numerical Analysis of Dynamic Combustion in HyShot Scramjet Combustor with a Transverse Fuel Injection
- 발행 : 2007.05.04
초록
This paper describes numerical efforts to investigate combustion characteristics of HyShot scramjet combustor, where gaseous hydrogen is transversely injected into a supersonic cross flow. The corresponding altitude, angle of attack, and equivalence ratio are 35-23 km,