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Transonic flow of moist air around thin airfoils.

机译:薄空气膜周围潮湿空气的跨音速流动。

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A new small-disturbance model for two-dimensional, steady, and diabatic transonic flow of moist air around a thin airfoil is presented. The study is based on theoretical analyses and numerical simulations. The condensation processes include the nonequilibrium and homogeneous condensation for purified supersaturated moist air and the equilibrium and heterogeneous condensation for moist air with foreign nuclei. The model explores the nonlinear interactions between the near-sonic speed of the flow, the small thickness ratio and angle of attack of the airfoil, and the small amount of water vapor in the air. The flow field is governed by a nonhomogeneous (extended) transonic small-disturbance (TSD) equation for the solution of the velocity perturbation potential coupled with the condensation equations. In the case where the nonequilibrium and homogeneous condensation occurs, the classical nucleation and condensation equations are reduced to a set of four ordinary differential equations for the calculation of the condensate (or sublimate) mass fraction. In the case where the equilibrium and heterogeneous condensation occurs, the condensate mass fraction can be expressed in terms of the velocity potential. The asymptotic analysis gives the similarity parameters that govern the flow problem in each case. An iterative numerical method which combines the type-sensitive difference scheme of Murman and Cole [14] for the solution of TSD equation with Simpson's integration rule for the estimation of condensate mass production is developed. The numerical scheme is studied for mesh convergence and also shows agreement of the pressure coefficient distribution, of the condensate mass fraction distribution, and of the water vapor pressure as a function of temperature with available results [23] from simulations using the Euler equations. The present work provides the theoretical understanding of two-dimensional transonic flows of moist air around thin airfoils with energy supply by the condensation.
机译:提出了一种新的小扰动模型,用于薄翼型周围二维,稳定且非绝热的湿空气跨音速流动。该研究基于理论分析和数值模拟。冷凝过程包括纯净过饱和湿空气的非平衡和均相冷凝,以及带有异核的湿空气的平衡和非均相冷凝。该模型探讨了气流的近音速,翼型的较小厚度比和迎角以及空气中少量的水蒸气之间的非线性相互作用。流场受非均匀(扩展)跨音速小扰动(TSD)方程控制,该方程用于求解速度扰动电势和凝聚方程。在发生不平衡和均相冷凝的情况下,经典的成核和冷凝方程式简化为一组四个常微分方程式,用于计算冷凝物(或升华物)的质量分数。在发生平衡凝结和非均相凝结的情况下,凝结质量分数可以用速度势来表示。渐进分析给出了控制每种情况下流动问题的相似性参数。开发了一种迭代数值方法,该方法将用于求解TSD方程的Murman和Cole [14]的类型敏感差分格式与用于估计凝结水量的辛普森积分规则相结合。研究了用于网格收敛的数值方案,并且还表明了压力系数分布,冷凝水质量分数分布以及水蒸气压力随温度的变化的一致性,可得到的结果[23]来自使用欧拉方程进行的模拟。本工作提供了薄空气翼周围湿空气的二维跨音速流动的理论理解,并通过冷凝提供能量。

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