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Low Pressure Turbine Flow Physics ProgramAs part of the collaborative NASA/industry/academia Low Pressure Turbine (LPT) Flow Physics program, smoke flow was visualized from a simulated low-pressure turbine experiment in NASA Lewis Research Center's CW-7 test facility. As shown in the photographs, a laminar separation bubble formed on the bottom flat surface. This is characteristic of the flows in a large-scale, low-pressure turbine operating under off-design conditions. A contoured upper wall was designed to generate a pressure distribution on a flat plate to match the suction surface pressure distribution from a generic low-pressure turbine blade.
Document ID
20050177151
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Shyne, Rickey J.
(NASA Lewis Research Center Cleveland, OH, United States)
Sohn, Ki-Hyeon
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 23, 2013
Publication Date
March 1, 1997
Publication Information
Publication: Research and Technology 1996
Subject Category
Research And Support Facilities (Air)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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