等离子体激励对飞行器流场影响的数值研究
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国家自然科学基金(51076168)


Numerical Investigation of the Effect of Plasma Actuation to Vehicle Flow-Filed
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    摘要:

    针对传统飞行器控制方式的缺点,采用小尺度等离子体流动控制技术对飞行器流场影响进行研究。在前 人的实验模型及飞行参数进行研究的基础上建立三维模型,采用数值仿真方法,研究了等离子体激励器位置和注入 能量大小对飞行器流场及表面压力分布的影响。仿真结果表明:等离子体与边界层的相互作用可改变飞行器外部激 波的初始结构,并在激励位置附近形成局部高压区;随着注入能量的增加,高压区峰值及作用范围分别扩大;等离 子体激励产生的扰动具有三维传播特性,对飞行器侧壁面甚至对整个壁面周向压力分布产生影响。

    Abstract:

    Aiming at the disadvantages of the traditional control method of vehicle, the plasma with little scale control technology is used to investigate the influence on vehicle flow-filed. Based on the researches of the former experiment’ model and fly parameters, established a three-dimensional vehicle model, and a numerical study of the flow fields and pressure distribution rules is accomplished with different position and energy deposition of plasma actuation. The simulative results indicate that the plasma actuation has an effect on the structure of the initial shock wave through the interaction between plasma and boundary layer. It also shows that there are high pressure region at the position of plasma actuation. As the energy deposition is increasing, the extent and peak value of high pressure region would be augmented. The perturbation evolution has a 3-D characteristic; the perturbation can spread abroad the surface and influence the side face and even the whole circumference pressure distribution

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冯伟,聂万胜,屠恒章,车学科.等离子体激励对飞行器流场影响的数值研究[J].,2011,30(11):20-23.

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  • 收稿日期:2013-02-01
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