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The unsteady loads and flow field on a maneuvering aircraft considerably differ from static conditions,especially for co......
Nose Micro-Blowing for Asymmetric Vortices Control on Blunt-Nose Slender Body at High Angle of Attac
The asymmetric vortices over blunt-nose slender body at high angles of attack result in random side force....
本文研究圆锥机身模型在迎角0°~90°范围内的气动力特性,采用边条控制技术,可获得所需要的控制力与控制力矩,通过边条的对称或单......
本文将双三角翼翼而测压试验结果与空间涡态观察测量结果进行了定性的相关对比分析,分析表明:垂直于双三角翼翼面的典型横截面上压力......