Show simple item record

contributor authorA. P. Morse
date accessioned2017-05-08T23:37:03Z
date available2017-05-08T23:37:03Z
date copyrightJanuary, 1991
date issued1991
identifier issn0889-504X
identifier otherJOTUEI-28608#98_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109451
description abstractA low turbulence Reynolds number k-ε model has been used in conjunction with an elliptic flow calculation procedure to obtain finite-difference solutions for radial outflow in the cavity formed between two plane corotating disks and an outer peripheral shroud. Air enters the cavity axially through a central hole in one of the disks and is assumed to leave via a uniform sink layer adjacent to the shroud. The main emphasis of the paper is the extension of the solution procedure to cover high rotational speeds, with rotational Reynolds numbers up to 107 . As a necessary prerequisite to this exercise, the turbulence model is validated by its good predictive accuracy of existing experimental data up to a maximum rotational Reynolds number of 1.1 × 106 .
publisherThe American Society of Mechanical Engineers (ASME)
titleApplication of a Low Reynolds Number k–ε Turbulence Model to High-Speed Rotating Cavity Flows
typeJournal Paper
journal volume113
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2927743
journal fristpage98
journal lastpage105
identifier eissn1528-8900
keywordsTurbulence
keywordsReynolds number
keywordsCavity flows
keywordsDisks
keywordsCavities
keywordsOutflow AND Flow (Dynamics)
treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 001
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record