The application of the proper orthogonal decomposition (POD) method to the vibration response of a cracked rotor system is investigated. The covariance matrices of the horizontal and vertical whirl amplitudes are formulated based on the numerical and experimental whirl response data for the considered cracked rotor system. Accordingly, the POD is directly applied to the obtained covariance matrices where the proper orthogonal values (POVs), and the proper orthogonal modes (POMs) are obtained for various crack depths, unbalance force vector angles, and rotational speeds. It is observed that both POVs and their corresponding POMs are highly sensitive to the appearance of the crack and the unbalance force angle direction in the neighborhoods of the critical rotational speeds. The sensitivity zones of the POVs and POMs to the crack propagation are found to be coinciding with the unstable zones found by the Floquet's theory of the considered cracked system.
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November 2018
Research-Article
Application of the Proper Orthogonal Decomposition Method for Cracked Rotors
Mohammad A. Al-Shudeifat,
Mohammad A. Al-Shudeifat
Aerospace Engineering Khalifa,
University of Science and Technology,
Abu Dhabi 127788, United Arab Emirates
e-mail: mohd.shudeifat@ku.ac.ae
University of Science and Technology,
Abu Dhabi 127788, United Arab Emirates
e-mail: mohd.shudeifat@ku.ac.ae
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Ayesha Al Mehairi,
Ayesha Al Mehairi
Aerospace Engineering Khalifa,
University of Science and Technology,
Abu Dhabi 127788, United Arab Emirates
e-mail: ayesha.almehairi@etic.ac.ae
University of Science and Technology,
Abu Dhabi 127788, United Arab Emirates
e-mail: ayesha.almehairi@etic.ac.ae
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Adnan S. Saeed,
Adnan S. Saeed
Aerospace Engineering,
Khalifa University of Science and Technology,
Abu Dhabi 127788, United Arab Emirates
e-mail: adnan.saeed@kustar.ac.ae
Khalifa University of Science and Technology,
Abu Dhabi 127788, United Arab Emirates
e-mail: adnan.saeed@kustar.ac.ae
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Shadi Balawi
Shadi Balawi
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Mohammad A. Al-Shudeifat
Aerospace Engineering Khalifa,
University of Science and Technology,
Abu Dhabi 127788, United Arab Emirates
e-mail: mohd.shudeifat@ku.ac.ae
University of Science and Technology,
Abu Dhabi 127788, United Arab Emirates
e-mail: mohd.shudeifat@ku.ac.ae
Ayesha Al Mehairi
Aerospace Engineering Khalifa,
University of Science and Technology,
Abu Dhabi 127788, United Arab Emirates
e-mail: ayesha.almehairi@etic.ac.ae
University of Science and Technology,
Abu Dhabi 127788, United Arab Emirates
e-mail: ayesha.almehairi@etic.ac.ae
Adnan S. Saeed
Aerospace Engineering,
Khalifa University of Science and Technology,
Abu Dhabi 127788, United Arab Emirates
e-mail: adnan.saeed@kustar.ac.ae
Khalifa University of Science and Technology,
Abu Dhabi 127788, United Arab Emirates
e-mail: adnan.saeed@kustar.ac.ae
Shadi Balawi
Contributed by the Design Engineering Division of ASME for publication in the JOURNAL OF COMPUTATIONAL AND NONLINEAR DYNAMICS. Manuscript received January 19, 2018; final manuscript received August 11, 2018; published online September 12, 2018. Assoc. Editor: Anindya Chatterjee.
J. Comput. Nonlinear Dynam. Nov 2018, 13(11): 111006 (9 pages)
Published Online: September 12, 2018
Article history
Received:
January 19, 2018
Revised:
August 11, 2018
Citation
Al-Shudeifat, M. A., Al Mehairi, A., Saeed, A. S., and Balawi, S. (September 12, 2018). "Application of the Proper Orthogonal Decomposition Method for Cracked Rotors." ASME. J. Comput. Nonlinear Dynam. November 2018; 13(11): 111006. https://doi.org/10.1115/1.4041234
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