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Study of the Roll Orientation Effects on Vortex Asymmetry on a Conical Forebody at High Angles of Incidence

机译:高入射角下前倾角对锥形前身涡流不对称性影响的研究

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Vortex asymmetry on conical forebodies at high angles of incidence results in large side force and yawing moments. Although the problem is well known and a number of flow control methods have been exploited, the nature of the instabilities causing vortex asymmetry and its variation with the roll orientation is not well understood. Experiments involving force and moment measurements and Particle Image Velocimetry on a conical forebody were performed at a Reynolds number of 0.22 million at various angles of incidence and roll orientations. Simulations involving a high-fidelity Navier-Stokes solver was performed near the tip region to better understand the flow physics. The results confirm the role of micro-imperfections near the tip region of conical forebody in developing vortex asymmetry and show that both the side force magnitude and the direction is very sensitive to roll orientation at high angles of attack.
机译:圆锥形前体在大入射角时涡旋不对称会导致较大的侧向力和偏航力矩。尽管该问题是众所周知的,并且已经开发了许多流动控制方法,但是引起涡旋不对称及其随侧倾方向变化的不稳定性的性质还不是很清楚。涉及在锥形前体上进行力和力矩测量以及粒子图像测速的实验,其雷诺数为22万,入射角和侧倾方向各不相同。在尖端区域附近进行了涉及高保真Navier-Stokes求解器的模拟,以更好地了解流场物理。结果证实了锥形前体尖端区域附近的微瑕疵在形成涡旋不对称中的作用,并表明侧向力的大小和方向都对高迎角下的侧倾方向非常敏感。

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