Numerical simulation of windward vortex shocks about supersonic slender bodies at high angles of attack 超声速大攻角旋成体迎风激波数值模拟
2.
Effects of leeside vortex isolation on pressure distribution over a high - alpha body of revolution 背风涡隔离对大攻角旋成体表面压力分布的影响
3.
The shm ( single hole microblowing ) as a new perturbation active control technique has been applied to the slender body with different model noses at zero sideslip and high angle of attack 摘要在亚临界流动范围内，对具有不同头部形状的尖拱形细长旋成体在无侧滑大迎角下进行单孔位微吹气扰动控制实验。
4.
The analyzed and contrasted results of the distribution of the surface pressure distributions and the sectional side forces with the former results of the slender body in the same flow conditions show that the shm ' s control effect to the slender body is due to that the two asymmetric vortices over the slender body model are sensitive to the nose perturbations 通过对物面压力分布、截面侧向力分布和以前细长旋成体结果的对比和分析，发现单孔位微吹气扰动对于细长旋成体横侧向控制作用在于模型头部背风侧非对称二涡结构对扰动的敏感性。
