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contributor authorK. P. Sarathy
date accessioned2017-05-08T23:13:16Z
date available2017-05-08T23:13:16Z
date copyrightApril, 1982
date issued1982
identifier issn1528-8919
identifier otherJETPEZ-26772#394_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95803
description abstractA three-dimensional inviscid time-marching calculation solving the unsteady Euler equations in a coordinate system rotating with the blade row has been developed, based on the Denton flow solver. This calculation was used to compute the flow field through the rotor of a transonic axial compressor and compared to measurements made with an advanced laser velocimeter at DFVLR. The comparison is made at design speed at pressure ratio corresponding to peak efficiency. Comparisons of the calculated and experimentally determined Mach number contours indicate excellent agreement in the entrance region where the viscous blockage effects are small. The methodology of the analysis is also described in this paper.
publisherThe American Society of Mechanical Engineers (ASME)
titleComputation of Three-Dimensional Flow Fields Through Rotating Blade Rows and Comparison With Experiment
typeJournal Paper
journal volume104
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3227291
journal fristpage394
journal lastpage400
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsComputation
keywordsRotating blades
keywordsPressure
keywordsEntrance region
keywordsEquations
keywordsMach number
keywordsLasers
keywordsMeasurement
keywordsCompressors
keywordsVelocimeters
keywordsDesign
keywordsRotors AND Blades
treeJournal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002
contenttypeFulltext


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