On the Physics of Heat Transfer and Aerodynamic Behavior of Separated Flow Along a Highly Loaded Low Pressure Turbine Blade Under Periodic Unsteady Wake Flow and Varying of Turbulence Intensity
Author:
Publisher
ASME International
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science
Link
http://heattransfer.asmedigitalcollection.asme.org/data/Journals/JHTRAO/27836/051703_1.pdf
Reference38 articles.
1. On the Physics of Flow Separation Along a Low Pressure Turbine Blade Under Unsteady Flow Conditions
2. Experimental Study of the Effect of Periodic Unsteady Wake Flow on Boundary Layer Development, Separation, and Reattachment Along the Surface of a Low Pressure Turbine Blade
3. 2004
4. Schobeiri, M. T., Öztürk, B., and Ashpis, D. , 2005, “Effect of Reynolds Number and Periodic Unsteady Wake Flow Condition on Boundary Layer Development, Separation, and Re-attachment Along the Suction Surface of a Low Pressure Turbine Blade,” ASME Paper No. GT2005-68600.
5. Schobeiri, M. T., Öztürk, B., and Ashpis, D. , 2005, “Intermittent Behavior of the Separated Boundary Layer Along the Suction Surface of a Low Pressure Turbine Blade Under Periodic Unsteady Flow Conditions,” ASME Paper No. GT2005-68603.
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