Prediction and Suppression of Low-Engine-Order Excitation of Axial Compressor Blisk Due to Measurement Probes
Author:
Affiliation:
1. Corporate Technology Division, Kawasaki Heavy Industries, Ltd.
2. Aerospace System Company, Kawasaki Heavy Industries, Ltd.
Publisher
Gas Turbine Society of Japan
Link
https://www.jstage.jst.go.jp/article/jgpp/15/4/15_vol15no4tp01/_pdf
Reference32 articles.
1. Srinivasan, A. V. " Flutter and Resonant Vibration Characteristics of Engine Blades." ASME. J. Eng. Gas Turbines Power. October 1997; 119(4): 742–775.
2. Bendiksen, O. O., and Friedmann, P. P. " The Effect of Bending-Torsion Coupling on Fan and Compressor Blade Flutter." ASME. J. Eng. Power. July 1982; 104(3): 617–623.
3. Judge, J., Pierre, C., and Mehmed, O. " Experimental Investigation of Mode Localization and Forced Response Amplitude Magnification for a Mistuned Bladed Disk ." ASME. J. Eng. Gas Turbines Power. October 2001; 123(4): 940–950.
4. Bréard, C., Green, J., and Imregun, M., “Low-engine-order excitation mechanisms in axial-flow turbomachinery” J. Propulsion and Power, 19(4), PP. 704-712. 2003.
5. Clark, W. S., and Hall, K. C. (February 1, 1999). " A Time-Linearized Navier–Stokes Analysis of Stall Flutter ." ASME J. Turbomach. July 2000; 122(3): 467–476.
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