LDV Measurements of Unsteady Flow in a Turbine Rotor
Author:
Affiliation:
1. National Institute of Advanced Industrial Science and Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-2742
Reference15 articles.
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2. Schulte, V., and Hodson, H. P., 1996, "Unsteady Wake-Induced Boundary Layer Transition in High Lift LPTurbines,"ASMEPaperNo.96-GT-486.
3. Murawski, C. G., Sondergaard, R., River, R. B., Vafai, K., Simon, T. W., and Volino, R. J., 1997, "Experimental Studyof theUnsteadyAerodynamics in a Linear Cascade with Low Reynolds Number Low Pressure Turbine Blades," ASME Paper No.97-GT-95.
4. Lake, J.P., King, P.I., and Rivir, R.B., 1999, "Reduction of Separation Losses on a Turbine Blade with Low Reynolds Number," AIAA Paper No.99-0242.
5. Turbine Separation Control Using Pulsed Vortex Generator Jets
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