摘要
介绍了用于飞行器尾喷流混合的主动流动控制技术,重点论述了脉冲射流强化飞行器尾喷流混合技术的应用状况。
出处
《飞航导弹》
北大核心
2010年第5期82-85,共4页
AERODYNAMIC MISSILE JOURNAL
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同被引文献12
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1苏长兵,宋慧敏,李应红,张朴,吴云,梁华.基于等离子体激励的圆柱绕流控制实验研究[J].实验流体力学,2006,20(4):45-48. 被引量:26
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6朱剑锋,黄国平,傅鑫,付勇.脉冲射流控制弯曲扩压管道流动分离的特点[J].航空动力学报,2015,30(12):2942-2948. 被引量:3
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