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contributor authorJ. M. Wetzel
contributor authorR. E. A. Arndt
date accessioned2017-05-08T23:44:39Z
date available2017-05-08T23:44:39Z
date copyrightJune, 1994
date issued1994
identifier issn0098-2202
identifier otherJFEGA4-27085#332_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113843
description abstractThe St. Anthony Falls Hydraulic Laboratory has been involved in the hydrodynamic design of large cavitation facilities, which require a high performance axial flow pump that is cavitation free to meet stringent design conditions. As cavitation has been shown to be the largest noise source in an otherwise well designed facility, it must be eliminated for the design range of flow conditions. To reduce the possibility of blade cavitation it is desirable to have a near uniform, or at least, a near symmetrical approach velocity distribution at the pump inlet. The design of flow facilities to achieve such an inflow was the subject of extensive investigations. These investigations consisted of both numerical and physical modeling of critical components in the test loop. The influence of these components, which included the contraction, diffuser, and turning vanes was carefully documented. The combination of the two modeling techniques will be demonstrated as an effective design tool for a high performance, hydrodynamic test facility.
publisherThe American Society of Mechanical Engineers (ASME)
titleHydrodynamic Design Considerations for Hydroacoustic Facilities: Part II—Pump Design Factors
typeJournal Paper
journal volume116
journal issue2
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.2910276
journal fristpage332
journal lastpage337
identifier eissn1528-901X
keywordsPumps
keywordsDesign
keywordsCavitation
keywordsFlow (Dynamics)
keywordsModeling
keywordsSymmetry (Physics)
keywordsDiffusers
keywordsNoise (Sound)
keywordsAxial flow
keywordsBlades
keywordsTest facilities
keywordsTurning vanes AND Inflow
treeJournal of Fluids Engineering:;1994:;volume( 116 ):;issue: 002
contenttypeFulltext


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