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首页> 外文期刊>International Review of Aerospace Engineering >The Impact Force Acting on a Normal Flat Plate Due to Non-Continuum Flow Issuing from Planner Exit with Different Speed Ratio
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The Impact Force Acting on a Normal Flat Plate Due to Non-Continuum Flow Issuing from Planner Exit with Different Speed Ratio

机译:由于不同速度比的刨床出口产生的非连续流动,冲击力作用在普通平板上

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This paper analysed the impact forces acting on a flat plate exposed normally to a rarefied plume issuing from a nozzle with a planner exit. The plate is assumed to be completely diffuse and the gaseous plume flow out of the exit is modelled with a Maxwellian distribution function, which was characterized with known number density, nonzero exit velocity, and temperature. The analytical collisionless flow results for drag force and shear force due to the impingement on the plate were derived. Effects of speed ratio, wall temperature, exit plume temperature, plate length and vertical distance between nozzle exit and plate center in the impact forces were studied. The results showed that the drag or shear force was directly proportional to the surface area of the flat plate. The drag and shear force increased as the speed ratio increased up to plate semi width of 0.7 m, then both forces decreased as the speed ratio increased up to the end of the plate length. The drag or shear force increased as the distance between the plate and nozzle exit decreased. In addition, the drag force increased as the plume exit temperature or plate temperature increased, while the shear force increased as the plume exit temperature increased. In considering the reflected particles from the plate or neglecting these particles; shear force was not affected, while drag force decreased when the reflected particles were neglected from the computation. Numerical simulation results obtained with the direct simulation Monte Carlo method validate the analytical collisionless flow solution for the surface pressure, shear stress distributions, and the impact forces.
机译:本文分析了作用在平板上的冲击力,该平板通常暴露于从带有规划器出口的喷嘴发出的稀疏羽流中。假定板是完全扩散的,并且用Maxwellian分布函数对流出出口的气态羽流建模,该函数的特征是已知的数密度,非零出口速度和温度。推导了由于撞击板而产生的阻力和剪力的无碰撞分析结果。研究了速度比,壁温,出口羽流温度,板长以及喷嘴出口与板中心之间的垂直距离对冲击力的影响。结果表明,阻力或剪切力与平板的表面积成正比。阻力和剪切力随着速度比的增加而增大,直至板的半宽度为0.7 m,然后两个力都随着速度比的增加而减小,直到板长度的尽头。阻力或剪切力随着板和喷嘴出口之间的距离的减小而增加。另外,拖曳力随着羽流出口温度或板温度的升高而增加,而剪切力随着羽流出口温度的升高而增加。在考虑从板反射的粒子或忽略这些粒子时;当计算中忽略了反射颗粒时,剪切力没有受到影响,而阻力减小了。通过直接模拟蒙特卡洛方法获得的数值模拟结果验证了表面压力,剪切应力分布和冲击力的解析无碰撞流动解。

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