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Numerical investigation on the effect of inlet conditions on the oblique shock system in a high-speed wind tunnel

机译:进气条件对高速风洞斜向冲击系统影响的数值研究

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The Present study is conducted to find out the best inlet conditions for designing process of a high-speed wind tunnel. The inlet conditions are appropriate for the cases that the real nozzle has not been calculated and downstream parts designers (such as test section and diffuser designers) need a reasonable upstream flow condition for their calculations. Inlet boundary condition of each case has been specified by User-Defined Function. The process of User-Defined Function (UDF) specification is time-consuming and is based on a try and error method. Several cases of inlet conditions have been designed and examined. The comparison of results is shown in terms of cross-sectional and axial distributions of parameters and contours of Mach number and static pressure. Finally, the 1.2 m-length Ogive curve with 0.5 degree initial angle and after that, the case of 1.2 m-length ducthave been chosen as the equivalent nozzles.
机译:进行本研究以找出用于高速风洞设计过程的最佳进气条件。入口条件适用于尚未计算实际喷嘴且下游零件设计人员(例如测试段和扩散器设计人员)需要合理的上游流动条件进行计算的情况。用户定义功能已指定每种情况的入口边界条件。用户定义功能(UDF)规范的过程非常耗时,并且是基于尝试和错误方法的。已经设计并检查了几种进气情况。结果的比较以参数的横截面和轴向分布以及马赫数和静压力的轮廓表示。最后,选择初始角度为0.5度的1.2 m长度的Ogive曲线,此后,选择1.2 m长度的导管作为等效喷嘴。

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