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首页> 外文期刊>Transactions of the Japan society for aeronautical and space sciences >Numerical Study of a Supersonic Jet Impinging on a Flat Plate in a Vacuum
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Numerical Study of a Supersonic Jet Impinging on a Flat Plate in a Vacuum

机译:超声射流在真空中撞击平板的数值研究

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Impingement of an axially symmetric free jet into a vacuum from a supersonic nozzle (M_e = 5) on a flat plate was studied based upon the Direct Simulation Monte Carlo method. Numerical simulations were carried out for hard-sphere molecules (for γ = 5/3) to examine the rarefaction effects of plume impingement in a vacuum environment. The distance from nozzle exit to the plate was four times the nozzle diameter. Results show that (1) a concaved plate shock is formed adjacent to the plate, (2) the compressed gas behind the plate shock expands and a supersonic plate jet is formed, and (3) the primary jet is then enveloped by the plate jet. The maximum value of the stagnation pressure on the plate is about 4.2% of the stagnation pressure of the primary jet. The maximum shear stress on the flat plate was found at R/H ≈ 0.17 for the case of Kn_D = 0.00625. This value may be slightly dependent on the Knudsen number. Present results showed a good agreement with the previous results of continuum theory and the results of experiments except for the rarefaction effects.
机译:基于直接模拟蒙特卡洛方法,研究了超音速喷嘴(M_e = 5)上的轴向对称自由射流对真空的撞击。对硬球分子(对于γ= 5/3)进行了数值模拟,以检查在真空环境中羽流撞击的稀疏效应。从喷嘴出口到板的距离是喷嘴直径的四倍。结果表明:(1)在板附近形成凹形板激波;(2)板激波后的压缩气体膨胀并形成超音速板喷流;(3)然后,主喷流被板喷流包围。平板上的停滞压力的最大值约为主喷嘴停滞压力的4.2%。对于Kn_D = 0.00625的情况,发现平板上的最大剪切应力为R / H≈0.17。该值可能略微取决于克努森数。除稀疏效应外,目前的结果与连续谱理论的先前结果和实验结果吻合良好。

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