Blade Loading Effects on Axial Turbine Tip Leakage Vortex Dynamics and Loss

Blade Loading Effects on Axial Turbine Tip Leakage Vortex Dynamics and Loss

umerical simulations have been carried out to define the loss generation mechanisms associated with tip leakage in un-shrouded axial turbines. Tip clearance vortex dynamics are a dominant feature of two mechanisms important in determining this loss: (i) decreased swirl velocity due to vortex line co...

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Bibliographic Details
Main Authors: Clemens, E. F., Gegg, S. G., Turner, E. R., Huang, Arthur C., Greitzer, Edward M., Tan, Choon S.
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Format: Article
Language:en_US
Published: ASME International 2014
Online Access:http://hdl.handle.net/1721.1/86369
https://orcid.org/0000-0001-9625-1020
https://orcid.org/0000-0002-8805-5289
https://orcid.org/0000-0002-8808-6632

Internet

http://hdl.handle.net/1721.1/86369
https://orcid.org/0000-0001-9625-1020
https://orcid.org/0000-0002-8805-5289
https://orcid.org/0000-0002-8808-6632

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