Modally Tuned Influence Coefficients for Low-Speed Balancing of Flexible Rotors
Author:
Affiliation:
1. Department of Mechanical Engineering, King Fahd University of Petroleum & Minerals, KFUPM Box 1767, Dhahran 31261, Saudi Arabia e-mail:
2. Data & Consulting Services, Schlumberger Dhahran Tech Valley, Dhahran 31261, Saudi Arabia e-mail:
Abstract
Publisher
ASME International
Subject
General Engineering
Link
http://asmedigitalcollection.asme.org/vibrationacoustics/article-pdf/doi/10.1115/1.4025995/6342702/vib_136_02_024501.pdf
Reference17 articles.
1. Ehrich, R., 1980, “High Speed Balancing Procedure,” 9th Turbomachinery Symposium, Turbolab, Texas A&M University, College Station, TX, pp. 25–31.
2. On the Isolation of Modes in the Balancing of Flexible Shafts;Proc. Inst. Mech. Eng.,1963
3. Calculation and Experiments on the Unbalance Response of a Flexible Rotor;ASME J. Ind. Ser. B,1967
4. A Theoretical Introduction to the Development of a Unified Approach to Flexible Rotor Balancing;J. Sound Vibr.,1980
5. Modal Balancing of Flexible Rotors Without Test Runs: An Experimental Investigation;J. Sound Vibr.,1983
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