In the present study, several control devices have been investigated in the framework of a high pressure compressor rotor using RANS simulations. The analysis of performance maps and of flow predictions leads to select the injection device located up-stream of the rotor tip, at the shroud in order to control the tip leakage flow. The high loss levels are reduced and the radial and azimuthal extension of the high loss area is smaller. Then the chosen flow control technique has been simulated using URANS and ZDES with the IGV passing wakes. The injection technique reduces the loss area and level, energizing and stabilizing the tip leakage vortex thanks to high momentum. So the vortex disruption is removed or at least delayed. Moreover, the influence of IGV passing wakes is reduced.
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ASME Turbo Expo 2014: Turbine Technical Conference and Exposition
June 16–20, 2014
Düsseldorf, Germany
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4561-5
PROCEEDINGS PAPER
Zonal Detached Eddy Simulation of Tip Leakage Flow Control in an Axial High Pressure Compressor
Julien Marty,
Julien Marty
Onera – The French Aerospace Lab, Meudon, France
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William Riéra,
William Riéra
Onera – The French Aerospace Lab, Meudon, France
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Lionel Castillon
Lionel Castillon
Onera – The French Aerospace Lab, Meudon, France
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Julien Marty
Onera – The French Aerospace Lab, Meudon, France
William Riéra
Onera – The French Aerospace Lab, Meudon, France
Lionel Castillon
Onera – The French Aerospace Lab, Meudon, France
Paper No:
GT2014-25150, V02BT39A003; 14 pages
Published Online:
September 18, 2014
Citation
Marty, J, Riéra, W, & Castillon, L. "Zonal Detached Eddy Simulation of Tip Leakage Flow Control in an Axial High Pressure Compressor." Proceedings of the ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. Volume 2B: Turbomachinery. Düsseldorf, Germany. June 16–20, 2014. V02BT39A003. ASME. https://doi.org/10.1115/GT2014-25150
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