The results of calculation show that the numerical procedure is reasonable and can be expended to predict the turbulent reacting flows in the annularcombustor.
计算结果表明计算方法合理,这计算程序进一步扩展,可用来预估环形燃烧室反应流流场。
2
The annular multi-hole radial jets have important effect on combustor liner.
环向径向射流对燃烧室火焰筒内的流场有着重要的影响。
3
Turbulent reactive flow in a short annularcombustor is simulated by changing the number and location of nozzle and swirler in combustor dome.