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Turbine tip clearance loss mechanisms

2013
Three-dimensional numerical simulations (RANS and URANS) were used to assess the impact of two specific design features, and of aspects of the actual turbine environment, on turbine blade tip loss. The calculations were carried out for a subsonic high pressure turbine stage. The loss mechanism examined is that due to tip clearance vortex mixing.
openaire   +1 more source

Effect of tip clearance on the cooling performance of a microchannel heat sink

International Journal of Heat and Mass Transfer, 2004
Seok Pil Jang
exaly  

Unsteady tip clearance flow in an isolated axial compressor rotor

Journal of Thermal Science, 2005
Weiguang Huang   +2 more
exaly  

Aeroacoustic investigation of a tip clearance flow

2007
Jacob, Marc   +3 more
openaire   +2 more sources

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