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Literaturverzeichnis<br />
98<br />
[1] J. Denton. Loss mechanisms in turbomachines. ASME Journal of Turbomachinery,<br />
115:621–656, October 1993. Issue 4.<br />
[2] H. Saathoff and U. Stark. Tip clearance flow induced endwall boundary layer separation<br />
in a single-stage axial-flow low-speed compressor. Proceedings of ASME Turbo Expo, (Paper<br />
number GT-2000-0501), 2000.<br />
[3] K. Suder and M. Celestina. Experimental and computational investigation of the tip<br />
clearance flow in a transonic axial compressor rotor. ASME Journal of Turbomachinery,<br />
118:218–229, April 1996. Issue 2.<br />
[4] J. Bae, K. Breuer, and C. Tan. Periodic unsteadiness of compressor tip clearance vortex.<br />
Proceedings of ASME Turbo Expo, (Paper number GT-2004-53015), 2004.<br />
[5] F. Lin, Z. Tong, S. Geng, J. Zhang, J. Chen, and C. Nie. A summary of stall warning and<br />
suppression research with micro tip injection. Proceedings of ASME Turbo Expo, (Paper<br />
number GT-2011-46118), 2011.<br />
[6] H. Schrapp. Experimentelle Untersuchungen zum Aufplatzen des Spaltwirbels in Axialverdichtern.<br />
PhD thesis, TU Braunschweig, 2008.<br />
[7] K. Yamada, M. Furukawa, T. Nakano, M. Inoue, and K. Funazaki. Unsteady threedimensional<br />
flow phenomena due to breakdown of tip leakage vortex in a transonic axial<br />
compressor. Proceedings of ASME Turbo Expo, (Paper number GT-2004-53745), 2004.<br />
[8] M. Smart and M. Kalkhoran. Flow model for predicting normal shock wave induced<br />
vortex breakdown. AIAA Journal, 35:1589–1596, October 1997.<br />
[9] C. Hah, D. Rabe, and A. Wadia. Effects of aerodynamic sweep on the development of tip<br />
leakage vortex and stall inception in transonic compressor rotors. Proceedings of International<br />
Symposium on Air Breathing Engines, (Paper number 2005-1142), 2005.<br />
[10] C. Hah, D. Rabe, and A. Wadia. Role of tip-leakage vortices and passage shock in stall<br />
inception in a swept transonic compressor rotor. Proceedings of ASME Turbo Expo, (Paper<br />
number GT-2004-53867), 2004.<br />
[11] N. Lambourne and D. Bryer. The bursting of leading edge vortices - some observations<br />
and discussion of the phenomenon. Aeronautical Research Council, (R and M No. 3282),<br />
1962. Issue 2.<br />
[12] S. Gbadebo, N. Cumpsty, and T. Hynes. Three-dimensional separations in axial compressors.<br />
ASME Journal of Turbomachinery, 127:331–339, April 2005. Issue 2.<br />
[13] V.-M. Lei, Z. Spakovszky, and E. Greitzer. A criterion for axial compressor hub-corner stall.<br />
ASME Journal of Turbomachinery, 130(Paper number 031006), July 2008. Issue 3.