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Experimental Study on the Magneto-aerodynamic Force Deflected by Magnetic Field Interaction in a Weakly-ionized Plasma Flow

机译:磁场相互作用在弱电离等离子体流动中偏转的磁空气动力学的实验研究

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By an electrodynamic flow control using a magnetic field interaction in a weakly ionized plasma flow, the aerodynamic force acting on hypersonic vehicles could be controlled without any mechanical architecture. The side force is generated on the symmetric body if the magnetic field is inclined against the body axis. The in-plane component of the side force based on the plane defined by the body axis and the magnetic pole is straightforwardly expected to generate because the magnetic field is no longer symmetry, and it was confirmed experimentally. On the other hand, the recent numerical study suggested that the out-plane component of the side force is also generated by the Hall effect even if the configuration such as the geometry and the magnetic field is symmetry. In the present study, the out-plane component of the side force acting on a magnetized model is experimentally measured utilizing the arcjet wind tunnel to verify the generation of it. As a result, it is confirmed that the out-plane force acts on the experimental model when the magnetic field is inclined against the body axis. This experimental result agrees with the numerical simulation.
机译:通过使用弱电离等离子体流动中的磁场相互作用的电动流动控制,可以控制作用在超音速车辆上的空气动力,而无需任何机械架构。如果磁场沿主体轴线倾斜,则在对称体上产生侧力。基于由主体轴线和磁极限定的平面的侧力的面内分量直接预期产生,因为磁场不再对称,并且实验证实。另一方面,近期数值研究表明,即使诸如几何形状和磁场是对称的,也是由霍尔效果产生侧力的外平面分量。在本研究中,采用在磁化模型上的侧力的外平面分量通过弧形风洞进行实验测量以验证它的产生。结果,确认在磁场沿主体轴线倾斜时,外平面力作用在实验模型上。该实验结果同意数值模拟。

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