Show simple item record

contributor authorD. Drikakis
contributor authorS. Tsangaris
date accessioned2017-05-08T23:41:45Z
date available2017-05-08T23:41:45Z
date copyrightMarch, 1993
date issued1993
identifier issn0098-2202
identifier otherJFEGA4-27073#115_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112183
description abstractNumerical simulation of compressible nozzle flows of real gas with or without the addition of heat is presented. A generalized real gas method, using an upwind scheme and curvilinear coordinates, is applied to solve the unsteady compressible Euler equations in axisymmetric form. The present method is an extension of a previous 2D method, which was developed to solve the problem for a gas having the general equation of state in the form p = p(ρ, i). In the present work the method is generalized for an arbitrary P-V-T equation of state introducing an iterative procedure for the determination of the temperature from the specific internal energy and the flow variables. The solution procedure is applied for the study of real gas effects in an axisymmetric nozzle flow.
publisherThe American Society of Mechanical Engineers (ASME)
titleReal Gas Effects for Compressible Nozzle Flows
typeJournal Paper
journal volume115
journal issue1
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.2910092
journal fristpage115
journal lastpage120
identifier eissn1528-901X
keywordsFlow (Dynamics)
keywordsNozzles
keywordsEquations of state
keywordsEquations
keywordsHeat
keywordsTemperature
keywordsComputer simulation AND Internal energy (Physics)
treeJournal of Fluids Engineering:;1993:;volume( 115 ):;issue: 001
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record