Numerical investigation of the influence of the camber distribution at the rotor tip on the efficiency at different tip clearances

Author:

Schrapp Henner,Fischer Denes,Ortmanns Jens,Goller Markus,Power Bronwyn

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference19 articles.

1. Chen, G.T.: Vortical structures in turbomachinery tip clearance flows. PhD thesis, Massachusetts Institute of Technology (1991)

2. Freeman, C.: Effect of tip clearance flow on compressor stability and engine performance. von Kármán Institut for Fluid Dynamics, Lecture series 1985-05 (1985)

3. Furukawa, M., Saiki, K., Yamada, K., Inoue, M.: Unsteady flow behavior due to breakdown of tip leakage vortex in an axial compressor rotor at near-stall conditions. In: Proceedings of ASME TurboExpo 2000, Munich, Paper No. 2000-GT-666 (2000)

4. Inoue, M., Kuroumaru, M.: Structure of tip clearance flow in an isolated axial compressor rotor. ASME J. Turbomach. 111, 250–256 (1989)

5. Lakshminarayana, B., Horlock, J.H.: Leakage and secondary flows in compressor cascade. Aeronautical Research Council Reports and Memoranda No. 3483 (1965)

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