航空工程进展
航空工程進展
항공공정진전
ADVANCES IN AERONAUTICAL SCIENCE AND ENGINEERING
2012年
2期
223-228
,共6页
亚燃冲压发动机%燃烧室%非均匀流%数值计算%燃烧效率%涡耗散概念
亞燃遲壓髮動機%燃燒室%非均勻流%數值計算%燃燒效率%渦耗散概唸
아연충압발동궤%연소실%비균균류%수치계산%연소효솔%와모산개념
ramjet%combustion chamber%nonuniform flow%numerical simulation%combustion efficiency%eddy dissipation concept
为研究人口非均匀流对亚燃燃烧室性能的影响,基于进气道出口试验测量数据,构造三种典型非均匀流型,对燃烧室进行三维数值计算,研究非均匀流对马赫数分布、温度场、燃油分布及燃烧效率的影响。结果表明:基于均匀流供油律,非均匀流影响燃烧室性能的机理是受流速主导作用,低速区域当量比偏高,高速区域当量比偏低。导致扩压段边区燃烧,烧蚀外环阻塞结构,而内圈高速区域燃烧组织效果欠佳。匹配供油律后,非均匀流燃烧性能有所改善,但难以达到均匀流水平。所以,提出了改进入口流均匀性及减弱非均匀流对燃烧不良影响的措施。
為研究人口非均勻流對亞燃燃燒室性能的影響,基于進氣道齣口試驗測量數據,構造三種典型非均勻流型,對燃燒室進行三維數值計算,研究非均勻流對馬赫數分佈、溫度場、燃油分佈及燃燒效率的影響。結果錶明:基于均勻流供油律,非均勻流影響燃燒室性能的機理是受流速主導作用,低速區域噹量比偏高,高速區域噹量比偏低。導緻擴壓段邊區燃燒,燒蝕外環阻塞結構,而內圈高速區域燃燒組織效果欠佳。匹配供油律後,非均勻流燃燒性能有所改善,但難以達到均勻流水平。所以,提齣瞭改進入口流均勻性及減弱非均勻流對燃燒不良影響的措施。
위연구인구비균균류대아연연소실성능적영향,기우진기도출구시험측량수거,구조삼충전형비균균류형,대연소실진행삼유수치계산,연구비균균류대마혁수분포、온도장、연유분포급연소효솔적영향。결과표명:기우균균류공유률,비균균류영향연소실성능적궤리시수류속주도작용,저속구역당량비편고,고속구역당량비편저。도치확압단변구연소,소식외배조새결구,이내권고속구역연소조직효과흠가。필배공유률후,비균균류연소성능유소개선,단난이체도균균류수평。소이,제출료개진입구류균균성급감약비균균류대연소불량영향적조시。
Based upon analyzing experiment data of air intake outlet, three types of nonuniform mass flux profile are constructed to investigate the impact on the chamber performance. A 3D numerical study of chamber flow is performed with these three profiles. The effects on Mach number distribution, temperature field, fuel distribution and combustion efficiency are studied. The results show that the nonuniform velocity caused by nonuniform mass flux is the essential effecting factor, together with the uniform fuel-feeding rule, the distribution of equivalence ratio is bad. The effecting mechanism is the equivalence ratio is higher in low speed area and lower in high- speed area. Low speed areas with higher equivalence ratio make the boundary zones of diffuser combust earlier and take a risk of burning the outer blockage structure. High-speed areas with relatively lower equivalence ratio lead to worse combustion effect. After adjusting the fuel-feeding rule, performance with nonuniform flow is im- proved, but hard to reach the level of uniform flow. Strategies of improving inlet flow uniformities and combustion quality are presented in the end.