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Flowfield Downstream of a Compressor Cascade with Tip Leakage

2014
An 8 blade, 7 passage linear compressor cascade with tip leakage was built. The flowfield downstream of the cascade was measured using four sensor hot-wire anemometers, from which the mean velocity field , the turbulence stress field and velocity spectra were obtained. Oil flow visualizations were done on the endwall underneath the blade row.
openaire   +1 more source

Influence of tip leakage flow and ejection on stall mechanism in a transonic tandem rotor

Aerospace Science and Technology, 2018
Le Han, Yanrong Wang
exaly  

Turbulence structure of a tip-leakage vortex wake

35th Aerospace Sciences Meeting and Exhibit, 1997
William Devenport   +9 more
openaire   +1 more source

Effect of a casing fence on the tip-leakage flow of an axial flow fan

International Journal of Heat and Fluid Flow, 2019
Keuntae Park, Haecheon Choi
exaly  

Effects of tip clearance size on the performance and tip leakage vortex in dual-rows counter-rotating compressor

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2015
Weixiong Chen, Siyuan Ren
exaly  

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