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contributor authorA. C. Aldo
contributor authorB. M. Argrow
date accessioned2017-05-08T23:47:34Z
date available2017-05-08T23:47:34Z
date copyrightJune, 1995
date issued1995
identifier issn0098-2202
identifier otherJFEGA4-27096#270_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/115521
description abstractRecently, dense gases have been investigated for many engineering applications such as for turbomachinery and wind tunnels. Supersonic nozzle design can be complicated by nonclassical dense-gas behavior in the transonic flow regime. In this paper, a method of characteristics (MOC) is developed for two-dimensional (planar) and axisymmetric flow of a van der Waals gas. A minimum length nozzle design code is developed that employs the MOC procedure to generate an inviscid wall contour. The van der Waals results are compared to perfect gas results to show the real-gas effects on the flow properties and inviscid wall contours.
publisherThe American Society of Mechanical Engineers (ASME)
titleDense Gas Flow in Minimum Length Nozzles
typeJournal Paper
journal volume117
journal issue2
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.2817140
journal fristpage270
journal lastpage276
identifier eissn1528-901X
keywordsGas flow
keywordsNozzles
keywordsDesign
keywordsFlow (Dynamics)
keywordsGases
keywordsEngineering systems and industry applications
keywordsTransonic flow
keywordsTurbomachinery AND Wind tunnels
treeJournal of Fluids Engineering:;1995:;volume( 117 ):;issue: 002
contenttypeFulltext


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