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

Kouremenos, DA; Krikkis, RN

dc.contributor.author	Kouremenos, DA	en
dc.contributor.author	Krikkis, RN	en
dc.date.accessioned	2014-03-01T01:07:47Z
dc.date.available	2014-03-01T01:07:47Z
dc.date.issued	1990	en
dc.identifier.issn	0961-3552	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/10171
dc.relation.uri	http://www.scopus.com/inward/record.url?eid=2-s2.0-45149140092&partnerID=40&md5=78f58ec895865691106eca88d827c925	en
dc.subject	compressible flow	en
dc.subject	Normal shock waves	en
dc.subject	refrigerant R22	en
dc.subject.classification	Engineering, Multidisciplinary	en
dc.title	A VMS/FORTRAN 77 program to compute the normal shock waves of refrigerant R22	en
heal.type	journalArticle	en
heal.language	English	en
heal.publicationDate	1990	en
heal.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. © 1990.	en
heal.publisher	ELSEVIER SCI LTD	en
heal.journalName	Advances in Engineering Software (1978)	en
dc.identifier.isi	ISI:A1990DY38800005	en
dc.identifier.volume	12	en
dc.identifier.issue	3	en
dc.identifier.spage	139	en
dc.identifier.epage	150	en