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Keywords: boundary layer method
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Journal Articles
Article Type: Research Papers
J. Turbomach. July 2009, 131(3): 031013.
Published Online: April 10, 2009
... − 10 deg to + 14.5 deg relative to design incidence. 05 04 2008 21 04 2008 10 04 2009 aerodynamics blades gas turbines turbomachinery MISES boundary layer method 2D cascade validation transonic off-design HPT incidence loss CFD Customers who purchase gas...