Spike-type stall inception in axial-flow compressors

ETC 2005 - 6th Conference on Turbomachinery: Fluid Dynamics and Thermodynamics

Volumn , Issue , 2005, Pages

  Deppe, A ^a   Saathoff, H ^a   Stark, U ^a  

^a TECHNICAL UNIVERSITY OF BRAUNSCHWEIG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW; AXIAL-FLOW COMPRESSORS; PRODUCT DESIGN; THERMODYNAMICS;

AIR INJECTION; EXPERIMENTAL INVESTIGATIONS; HIGH FREQUENCY HF; LOW SPEED COMPRESSOR; PRESSURE FIELD; ROTATING STALLS; STABLE OPERATION; STALL INCEPTION;

INLET FLOW;

EID: 84925427888     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

1. Brodersen, S., Wulff, D., 1992, \Measurements of the pressure and velocity distribution in low-speed turbomachinery by means of high-frequency pressure transducers," ASME Journal of Turbomachinery, Vol. 114, pp. 100-107.
2. Camp, T. R., Day, I. J., 1997, \A study of spike and modal stall phenomena in a low-speed axial compressor," ASME Journal of Turbomachinery, Vol. 120, pp. 393-401.
3. Deppe, A., Saathoff, H., Stark, U., 2004, \Stall inception phenomena in three single-stage low-speed axial compressors," Proceedings of the 10th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC, Honolulu, Hawaii, 2004.
4. Dobat, A., Saathoff, H., Wulff, D., 2001, \Experimentelle Untersuchungen zur Entstehung von Rotating Stall in Axialventilatoren," VDI-Berichte Nr. 1591, S. 345-360.
5. Furukawa, M., Saiki, K., Yamada, K., Inoue, M., 2000, \Unsteady ow behavior due to breakdown of tip leakage vortex in an axial compressor rotor at near-stall condition," ASME Paper No. 2000-GT-666.
6. Inoue, M., Kuroumaru, M., 1989, \Structure of tip clearance ow in an isolated axial ow compressor rotor," ASME Journal of Turbomachinery, Vol. 111, pp. 250-256.
7. Inoue, M., Kuroumaru, M., Iwamoto, T., Ando, Y., 1991, \Detection of rotating stall precursor in isolated axial ow compressor rotors," ASME Journal of Turbomachinery, Vol. 113, pp. 281-289.
8. Le Bot, Y., Paulon, J., Belaygue, P., 1970, \Theoretical and experimental determination of pressure losses in a single-stage axial ow compressor," ASME Journal of Engineering for Power, Vol. 92, pp. 407-414.
9. McDougall, N. M., 1988, \Stall inception in axial compressors," Ph. D. Dissertation, University of Cambridge.
10. Moore, F. K., Greitzer, E. M., 1986, \A theory of post-stall transients in axial compression systems. Parts I & II," ASME Journal of Engineering for Gas Turbines and Power, Vol. 108, pp. 68-76 & pp. 231-239.
11. Rohdenburg, M., Kosyna, G., 2001, \Experimentelle Bestimmung der Grenzschichtparameter von Axialventilatorstufen als Basis für Kennfeldberechnungen," VDI-Berichte Nr. 1591, S. 361-376.
12. Rohdenburg, M., 2003, \Kennfeldberechnungsverfahren für Axialventilatoren mit Berücksichtigung der Naben-und Gehäusegrenzschichten," Mitteilungen des Peiderer-Instituts für Strömungsmaschinen, Verlag und Bildarchiv W. H. Faragallah, Heft 8, (Dissertation, TU Braunschweig).
13. Saathoff, H., Stark, U., 2001, \Tip clearance ow in a low-speed compressor and cascade," Conference Proceedings, 4th European Conference on Turbomachinery -Fluid Dynamics and Thermodynamics, Firenze, Italy, pp. 81-91.
14. Saathoff, H., 2001, \Rotor-Spaltströmungen in Axialverdichtern," ZLR-Forschungsbericht 2001-05 (Dissertation, TU Braunschweig).
15. Saathoff, H., Deppe, A., Stark, U., Rohdenburg, M., Rohkamm, H.,Wulff, D., Kosyna, G., 2003, \Steady and unsteady casing wall ow phenomena in a single-stage low-speed compressor at part-load conditions," International Journal of Rotating Machinery, Vol. 9, pp. 327-335.
16. Vo, H. D., 2001, \Role of tip clearance ow on axial compressor stability," Ph. D. Dissertation, Massachusetts Institute of Technology.
17. Werlé, H., Gallon, M., 1977, \Maquette Hydraulique de Turbomachine," La Recherche Aérospatiale, Vol. 5, pp. 267-288.