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 : 2007.05.04
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,