Journal of Thermal Science | Vol.29, Issue.3 | 2020-05-31 | Pages 763-771
Efficient Determination of Turbomachinery Blade Aero-Damping Curves for Flutter Assessment via Trigonometric Interpolation
Proposed in the paper is a trigonometric interpolation method for efficient determination of turbomachinery blade aero-damping curves which are required in
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Efficient Determination of Turbomachinery Blade Aero-Damping Curves for Flutter Assessment via Trigonometric Interpolation
Proposed in the paper is a trigonometric interpolation method for efficient determination of turbomachinery blade aero-damping curves which are required in
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trigonometric interpolation method efficient determination of turbomachinery blade aerodamping curves
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Xiuquan Huang,Dingxi Wang,.Efficient Determination of Turbomachinery Blade Aero-Damping Curves for Flutter Assessment via Trigonometric Interpolation. 29 (3),763-771.
Ekici K., Hall K.C., Kielb R.E.. Harmonic balance analysis of blade row interactions in a transonic compressor. Journal of Propulsion and Power, 2010, 26(2)): 335–343.
Yang Z., Mavriplis D.J.. Time spectral method for quasi-periodic unsteady computation on unstructured meshes. AIAA Paper 2010-5034, 2006.
He L., Ning W.. An efficient approach for analysis of unsteady viscous flows in turbomachines. AIAA Journal, 1998, 36(11)): 2005–2012.
Vogel K., Naidu A.D., Fischer M.. Comparison of the influence coefficient method and travelling wave mode approach for the calculation of aerodynamic damping of centrifugal compressors and axial turbines. In Proceedings of ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition, 2017, Paper No: GT2017-64643, V07BT36A022.
Wang D., Huang X.. Solution stabilization and convergence acceleration for the harmonic balance equation system. Journal of Engineering for Gas Turbines and Power, 2017, 139(9)): 092503.
Hall K., Ekicib K., Thomas J.P., Dowell E.H.. Harmonic balance methods applied to computational fluid dynamics problems. International Journal of Computational Fluid Dynamics, 2013, 27(2)): 52–67.
Lane F.. System mode shapes in the flutter of compressor blade rows. Journal of the Aeronautical Sciences, 1956, 23(1)): 54–66.
Hall K., Thomas J., Clark W.. Computation of unsteady nonlinear flows in cascades using a harmonic balance technique. AIAA Journal, 2002, 40(5)): 879–886.
Hsu K., Hoyniak D.. A fast influence coefficient method for linearized flutter and forced-response analysis. In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. 2011. DOI: https://doi.org/10.2514/6.2011-229.
Huang X., He L., Bell D.L.. Experimental and computational study of oscillating turbine cascade and influence of part-span shrouds. ASME Journal of Fluids Engineering, 2009, 131(5)): 051102.
Yang H., He L.. Experiment study on linear compressor cascade with three-dimensional blade oscillation. Journal of Propulsion and Power, 2004, 20(1)):180–188.
Su X., Yuan X.. Implicit solution of time spectral method for periodic unsteady flows. International Journal for Numerical Methods in Fluids, 2010, 63: 860–876.
Hall K., Lorence C.. Calculation of three-dimensional unsteady flows in turbomachinery using the linearized harmonic Euler equations. Journal of Turbomachinery, 1993, 115(4)):800–809.
Sicot F., Puigt G., Montagnac M.. Block-Jacobi implicit algorithms for the time spectral method. AIAA Journal, 2008, 2(12)): 3080–3089.
Ma C., Su X., Gou J., Yuan X.. Runge-Kutta/implicit scheme for the solution of time spectral method. In ASME Paper GT2014-26474, 2014.
Hanamura Y., Tanaka H.. A simplified method to measure unsteady forces acting on the vibrating blades in a cascade. Bulletin of the JSME, 1980, 23(180)): 880–887.
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