Show simple item record

contributor authorM. Ishida
contributor authorY. Senoo
date accessioned2017-05-08T23:11:05Z
date available2017-05-08T23:11:05Z
date copyrightApril, 1981
date issued1981
identifier issn1528-8919
identifier otherJETPEZ-26765#271_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94520
description abstractThe pressure distribution along the shroud is measured for three types of centrifugal impeller at seven different values of tip clearance each. The change of input power due to a change of tip clearance is related to the effective blockage at the impeller tip. Since the change of input power is little for the test cases, the variation of local pressure gradient along the shroud is mostly attributed to the change of local pressure loss. The local pressure loss is related to the local tip clearance ratio and to the local pressure gradient based on the deceleration of relative velocity in the impeller. Since the local pressure gradient is largest near the throat of the impeller, for many impellers the clearance ratio at the throat is used as the representative value. The tip clearance loss is related to the clearance ratio and the pressure rise based on the deceleration of relative velocity in the impeller. A good correlation is observed in all cases at various flow rate.
publisherThe American Society of Mechanical Engineers (ASME)
titleOn the Pressure Losses Due to the Tip Clearance of Centrifugal Blowers
typeJournal Paper
journal volume103
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3230717
journal fristpage271
journal lastpage278
identifier eissn0742-4795
keywordsPressure
keywordsClearances (Engineering)
keywordsImpellers
keywordsPressure gradient AND Flow (Dynamics)
treeJournal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 002
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record