fuel-rich flame

基本解释

Experimental investigation on supersonic combustion of kerosene was conducted using fuel-rich hot gas as pilot flame on direct-connect supersonic combustion facility.
對採用高溫富油燃氣作引導火焰的煤油超聲速燃燒進行了研究。
The combustion wave temperature profiles and flame structures of fuel-rich propellant containing boron are measured by using W-Re micro-thermal couple and flame photo technique.
通過微熱電偶測溫和火焰單幅照相技術測試了含硼富燃料推進劑燃燒波溫度分佈及燃燒火焰結搆；
The combustion wave temperature profiles and the flame structures of fuel-rich propellant based on boron were measured by using W-Re micro-thermal couple and flame photo technique.
通過微熱電偶測溫和火焰單幅照相技術分別測試含硼富燃料推進劑燃燒波溫度分佈及燃燒火焰結搆；