A new method is developed for the forced response analysis of mistuned bladed disks manufactured from anisotropic materials and mistuned by different orientations of material anisotropy axes. The method uses (i) sector finite element (FE) models of anisotropic bladed disks and (ii) FE models of single blades and allows the calculation of displacements and stresses in a mistuned assembly. A high-fidelity reduction approach is proposed which ensures high-accuracy modeling by introducing an enhanced reduction basis. The reduction basis includes the modal properties of specially selected blades and bladed disks. The technique for the choice of the reduction basis has been developed, which provides the required accuracy while keeping the computation expense acceptable. An approach for effective modeling of anisotropy-mistuned bladed disk without a need to create a FE model for each mistuning pattern is developed. The approach is aimed at fast statistical analysis based on Monte Carlo simulations. All components of the methodology for anisotropy-mistuned bladed disks are demonstrated on the analysis of models of practical bladed disks. Effects of anisotropy mistuning on forced response levels are explored.
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February 2018
Research-Article
Analysis of Forced Response for Bladed Disks Mistuned by Material Anisotropy Orientation Scatters
Chaoping Zang,
Chaoping Zang
Jiangsu Province Key Laboratory of
Aerospace Power System,
Nanjing University of
Aeronautics and Astronautics,
Nanjing 210016, China
e-mail: c.zang@nuaa.edu.cn
Aerospace Power System,
Nanjing University of
Aeronautics and Astronautics,
Nanjing 210016, China
e-mail: c.zang@nuaa.edu.cn
Search for other works by this author on:
Yuanqiu Tan,
Yuanqiu Tan
Jiangsu Province Key Laboratory of
Aerospace Power System,
Nanjing University of
Aeronautics and Astronautics,
Nanjing 210016, China
e-mail: y.tan@nuaa.edu.cn
Aerospace Power System,
Nanjing University of
Aeronautics and Astronautics,
Nanjing 210016, China
e-mail: y.tan@nuaa.edu.cn
Search for other works by this author on:
E. P. Petrov
E. P. Petrov
School of Engineering and Informatics,
University of Sussex,
Brighton BN1 9QT, UK
e-mail: y.petrov@sussex.ac.uk
University of Sussex,
Brighton BN1 9QT, UK
e-mail: y.petrov@sussex.ac.uk
Search for other works by this author on:
Chaoping Zang
Jiangsu Province Key Laboratory of
Aerospace Power System,
Nanjing University of
Aeronautics and Astronautics,
Nanjing 210016, China
e-mail: c.zang@nuaa.edu.cn
Aerospace Power System,
Nanjing University of
Aeronautics and Astronautics,
Nanjing 210016, China
e-mail: c.zang@nuaa.edu.cn
Yuanqiu Tan
Jiangsu Province Key Laboratory of
Aerospace Power System,
Nanjing University of
Aeronautics and Astronautics,
Nanjing 210016, China
e-mail: y.tan@nuaa.edu.cn
Aerospace Power System,
Nanjing University of
Aeronautics and Astronautics,
Nanjing 210016, China
e-mail: y.tan@nuaa.edu.cn
E. P. Petrov
School of Engineering and Informatics,
University of Sussex,
Brighton BN1 9QT, UK
e-mail: y.petrov@sussex.ac.uk
University of Sussex,
Brighton BN1 9QT, UK
e-mail: y.petrov@sussex.ac.uk
Contributed by the Structures and Dynamics Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received October 16, 2016; final manuscript received July 7, 2017; published online October 10, 2017. Assoc. Editor: Alexandrina Untaroiu.
J. Eng. Gas Turbines Power. Feb 2018, 140(2): 022503 (12 pages)
Published Online: October 10, 2017
Article history
Received:
October 16, 2016
Revised:
July 7, 2017
Citation
Zang, C., Tan, Y., and Petrov, E. P. (October 10, 2017). "Analysis of Forced Response for Bladed Disks Mistuned by Material Anisotropy Orientation Scatters." ASME. J. Eng. Gas Turbines Power. February 2018; 140(2): 022503. https://doi.org/10.1115/1.4037863
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