Experiments in Active Control of Stall on an Aeroengine Gas Turbine
Author:
Affiliation:
1. Rolls-Royce plc, Derby, United Kingdom
2. Whittle Laboratory, Cambridge University, Cambridge, United Kingdom
3. MAS Research Ltd., 8 Pentlands Court, Pentlands Close, Cambridge, United Kingdom
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/120/4/637/5641939/637_1.pdf
Reference10 articles.
1. Day I. J. , 1993, “Active Suppression of Rotating Stall and Surge in Axial Compressors,” ASME JOURNAL OF TURBOMACHINERY, Vol. 115, pp. 40–47.
2. Day I. J. , and FreemanC., 1994, “The Unstable Behavior of Low and High-Speed Compressors,” ASME JOURNAL OF TURBOMACHINERY, Vol. 116, pp. 194–201.
3. Eveker, K. M., Gysling, D. L., Nett, C. N., and Sharma, O. P., 1995, “Integrated Control of Rotating Stall and Surge in Aeroengines,” SPIE Vol. 2494 (Proc. Conference “Sensing, Actuation and Control,” Orlando, FL, Apr. 17–18), pp. 21–35.
4. Ffowcs Williams J. E. , and HuangX. Y., 1989, “Active Stabilisation of Compressor Surge,” Journal of Fluid Mechanics, Vol. 204, pp. 245–262.
5. Freeman, C., and Wilson, A. G., 1993, “Stall Inception and Post Stall Transients in an Aero Engine Axial Flow Compressor,” presented at IMechE Seminar on Turbo Compressor and Fan Stability, London, Apr. 8.
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