Show simple item record

contributor authorT. T. Ng
contributor authorD. R. Otis
date accessioned2017-05-08T23:06:57Z
date available2017-05-08T23:06:57Z
date copyrightDecember, 1979
date issued1979
identifier issn0098-2202
identifier otherJFEGA4-26952#491_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92266
description abstractA radial ejector with two degrees of geometric control is constructed and tested at pressures ranging from 0.7 to 1.5 atmospheres and entrainment ratios ranging from 0 to 2. Maximum efficiencies of 16 percent were obtained, and performance could be maintained over a range of pressures by changing the position of the “spool,” an element defining the nozzle contours and flow areas. This design offers potential for applications with varying pressure and flow conditions where feedback control systems can continuously adjust the ejector geometry for maximum performance.
publisherThe American Society of Mechanical Engineers (ASME)
titleExperimental Investigation of a Variable Geometry, Radial Ejector
typeJournal Paper
journal volume101
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3449016
journal fristpage491
journal lastpage494
identifier eissn1528-901X
keywordsEjectors
keywordsGeometry
keywordsFlow (Dynamics)
keywordsDesign
keywordsNozzles
keywordsFeedback AND Pressure
treeJournal of Fluids Engineering:;1979:;volume( 101 ):;issue: 004
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record