试验研究了主、径向涡流器旋流数、面积比、套筒扩张角等参数对双旋流进气装置冷态流场的影响。
The effects of swirl number of primary swirler and radial swirler, area ratio and sleeve divergence angle on the cold flow field of double swirl air intake were investigated.
计算了旋成体大迎角涡流和带底部喷流的绕流场。
Numerical investigation of base jet interaction in a supersonic external flow;
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