This paper focuses on extending an earlier investigation on the systematic and rational consideration of uncertainty in reduced order models of rotordynamics systems. The current effort concentrates on the consistent introduction of uncertainty in mass properties on the modal mass and gyroscopic matrices and on the unbalance force vector. The uncertainty in mass is separated into uncertainty that maintains the rotor symmetry and the one which disrupts it. Both types of uncertainties lead to variations in the system modal matrices but only the latter induces an unbalance. Accordingly, the approach permits the selection of separate levels on the uncertainty on the system properties (e.g., natural frequencies) and on the unbalance. It was first found that the unbalanced response is increased by considering the uncertainty in the rotor modal mass matrices. It was next noted that the approach presented not only permits the analysis of uncertain rotors but it also provides a computational framework for the assessment of various balancing strategies. To demonstrate this unique feature, a numerical experiment was conducted in which a population of rotors were balanced at low speed and their responses were predicted at their first critical speed. These response predictions were carried with the uncertainty in the system modal mass matrices but with or without the balancing weights effects on these matrices. It was found that the balancing at low speed may, in fact, lead to an increase in both the mean and 95th percentile of the response at critical speed.
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June 2014
Research-Article
Nonparametric Stochastic Modeling of Structural Uncertainty in Rotordynamics: Unbalance and Balancing Aspects
Raghavendra Murthy,
Raghavendra Murthy
Mem. ASME
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: rnmurthy@asu.edu
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: rnmurthy@asu.edu
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Joseph C. Tomei,
Joseph C. Tomei
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: jctomei@asu.edu
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: jctomei@asu.edu
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X. Q. Wang,
X. Q. Wang
Mem. ASME
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: xiaoquan.wang.1@asu.edu
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: xiaoquan.wang.1@asu.edu
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Marc P. Mignolet,
Marc P. Mignolet
Fellow ASME
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: marc.mignolet@asu.edu
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: marc.mignolet@asu.edu
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Aly El-Shafei
Aly El-Shafei
Mem. ASME
Design and Production,
Cairo University,
e-mail: elshafei@gmail.com
Department of Mechanical
Design and Production,
Cairo University,
Giza 12316, Egypt
e-mail: elshafei@gmail.com
Search for other works by this author on:
Raghavendra Murthy
Mem. ASME
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: rnmurthy@asu.edu
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: rnmurthy@asu.edu
Joseph C. Tomei
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: jctomei@asu.edu
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: jctomei@asu.edu
X. Q. Wang
Mem. ASME
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: xiaoquan.wang.1@asu.edu
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: xiaoquan.wang.1@asu.edu
Marc P. Mignolet
Fellow ASME
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: marc.mignolet@asu.edu
SEMTE,
Faculties of Mechanical and Aerospace Engineering,
Arizona State University,
Tempe, AZ 85287
e-mail: marc.mignolet@asu.edu
Aly El-Shafei
Mem. ASME
Design and Production,
Cairo University,
e-mail: elshafei@gmail.com
Department of Mechanical
Design and Production,
Cairo University,
Giza 12316, Egypt
e-mail: elshafei@gmail.com
Contributed by the Structures and Dynamics Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received November 3, 2013; final manuscript received December 3, 2013; published online February 11, 2014. Editor: David Wisler.
J. Eng. Gas Turbines Power. Jun 2014, 136(6): 062506 (12 pages)
Published Online: February 11, 2014
Article history
Received:
November 3, 2013
Revision Received:
December 3, 2013
Citation
Murthy, R., Tomei, J. C., Wang, X. Q., Mignolet, M. P., and El-Shafei, A. (February 11, 2014). "Nonparametric Stochastic Modeling of Structural Uncertainty in Rotordynamics: Unbalance and Balancing Aspects." ASME. J. Eng. Gas Turbines Power. June 2014; 136(6): 062506. https://doi.org/10.1115/1.4026166
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