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Use of Blade Lean in Turbomachinery RedesignBlade lean is used to improve the uniformity of exit flow distributions from turbomachinery blading. In turbines, it has been used to control secondary flows by tailoring blade turning to reduce flow overturning and underturning and to create more uniform loss distributions from hub to shroud. In the present study, the Pump Consortium centrifugal impeller has been redesigned using blade lean. The flow at the exit of the baseline impeller had large blade-to-blade variations, creating a highly unsteady flow for the downstream diffuser. Blade lean is used to redesign the flow to move the high loss fluid from the suction side to the hub, significantly reducing blade-toblade variations at the exit.
Document ID
19950017205
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Moore, John
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Moore, Joan G.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Lupi, Alex
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1993
Publication Information
Publication: NASA. Marshall Space Flight Center, Eleventh Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 1
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
95N23625
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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