A VMS/FORTRAN 77 program to compute the normal shock waves of refrigerant R22

D.A. Kouremenos, R.N. Krikkis
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Abstract

When one-dimensional supersonic compressible flow undergoes a sudden retardation, a normal shock wave may occur. After the shock wave, the fluid properties can be obtained if continuity, momentum and energy balance laws are used. The method to compute the thermal and caloric properties of the fluid is explained in brief. A suitable FORTRAN 77 computer code is proposed, developed, tested and run with the operating system VMS on a MicroVAX II. With minor changes, it can run with MS-DOS on a PC/XT. The refrigerant R22 has been used as a fluid. Its thermal and caloric equation of state and the corresponding values are given in the following subroutines. Some results are given to check the code by potential users.

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一个用于计算R22制冷剂正常激波的VMS/FORTRAN 77程序
当一维超声速可压缩流发生突然减速时,会产生正常的激波。利用连续定律、动量定律和能量平衡定律,可以得到激波后流体的性质。简要说明了流体热、热特性的计算方法。提出了一种适合的FORTRAN 77计算机代码,并在MicroVAX II操作系统VMS上进行了开发、测试和运行。稍加改动,它就可以在PC/XT上与MS-DOS一起运行。制冷剂R22已作为流体使用。它的热和热量状态方程及相应的值在下面的子程序中给出。给出一些结果供潜在用户检查代码。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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