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contributor authorS. Kangovi
contributor authorR. H. Page
date accessioned2017-05-08T23:07:03Z
date available2017-05-08T23:07:03Z
date copyrightJune, 1979
date issued1979
identifier issn0098-2202
identifier otherJFEGA4-26944#230_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92318
description abstractThe flow past a downstream facing annular step was experimentally investigated in the Mach range of 0.1 to 0.95. The approaching flow was steady and uniform. The boundary layer ahead of the step was turbulent. The upstream influence of the step and the variation of base pressure and recovery pressure with the reference Mach number are described. Results of hot-wire measurements in the shear layer and the locations of reattachment and secondary separation points are also reported.
publisherThe American Society of Mechanical Engineers (ASME)
titleSubsonic Turbulent Flow Past a Downstream Facing Annular Step
typeJournal Paper
journal volume101
journal issue2
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3448940
journal fristpage230
journal lastpage235
identifier eissn1528-901X
keywordsTurbulence
keywordsFoundry coatings
keywordsPressure
keywordsFlow (Dynamics)
keywordsMach number
keywordsSeparation (Technology)
keywordsMeasurement
keywordsShear (Mechanics)
keywordsBoundary layers AND Wire
treeJournal of Fluids Engineering:;1979:;volume( 101 ):;issue: 002
contenttypeFulltext


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