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Some Scenarios for Transition on Turbomachinery BladingMeasurements on transition under different levels of adverse pressure gradient and free-stream turbulence level are described. This extensive series of investigations, which was predicated on intermittency measurement techniques, has resulted in correlations for transition length and turbulent spot formation rate. These correlations rae intended to be used in conjunction with boundary layer prediction methods and examples are given of such predictions. More effective predictions of the transition region, especially under conditions of variable pressure gradient, are dependent on a more comprehensive understanding of transition and spot behavior. It is expected that this will result in improved transition modeling.
Document ID
20070038968
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Gostelow, J. P.
(Sydney Univ. Australia)
Date Acquired
August 24, 2013
Publication Date
March 1, 2007
Publication Information
Publication: Minnowbrook I: 1993 Workshop on End-Stage Boundary Layer Transition
Subject Category
Aerodynamics
Distribution Limits
Public
Copyright
Public Use Permitted.
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