Journal of the Korean Society of Combustion (한국연소학회지)
- Volume 12 Issue 2
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- Pages.1-9
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- 2007
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- 1226-0959(pISSN)
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- 2466-2089(eISSN)
Numerical Analysis of Dynamic Combustion in HyShot Scramjet Combustor with a Transverse Fuel Injection
수직 연료 분사기구를 포함하는 HyShot 스크램제트 연소기의 동적 연소 유동해석
- Published : 2007.06.30
Abstract
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,