Computation Velocity, Pressure, Temperature Profiles in Cryogenic Turboexpander

Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/205

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DC Field	Value	Language
dc.contributor.author	Ghosh, S K	-
dc.contributor.author	Seshaiah, N	-
dc.contributor.author	Sahoo, R K	-
dc.contributor.author	Sarangi, S K	-
dc.date.accessioned	2006-01-15T07:11:14Z	-
dc.date.available	2006-01-15T07:11:14Z	-
dc.date.issued	2006	-
dc.identifier.citation	Proceedings of the 18th National and 7th ISHMT-ASME Heat and Mass Transfer Conference, January 4-6, 2006, IIT-Guwahati, India P 2015-2022	en
dc.identifier.uri	http://hdl.handle.net/2080/205	-
dc.description	Copyright for this article belongs to IIT-Guwahati, India	en
dc.description.abstract	An indigenous programme on design and development of a cryogenic turboexpander has been taken up at NIT, Rourkela. This paper presents the detailed computational procedure for determining the velocity, pressure and temperature profiles in the turbine wheel, nozzle and diffuser of the turboexpander. The procedure allows any arbitrary combination of fluid species, inlet conditions and expansion ratio, the fluid properties being properly taken care of in the relevant equations. The computational process is illustrated with an example.	en
dc.format.extent	242262 bytes	-
dc.format.mimetype	application/pdf	-
dc.language.iso	en	-
dc.publisher	IIT-Guwahati, India	en
dc.subject	Turboexpander	en
dc.subject	pressure	en
dc.subject	Temperature	en
dc.subject	Velocity	en
dc.title	Computation Velocity, Pressure, Temperature Profiles in Cryogenic Turboexpander	en
dc.type	Article	en
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