Bifurcation analysis for vibrations of a turbine blade excited by air flows

[1]  Y Bichiou,et al.  Nonlinear aeroelastic characterization of wind turbine blades , 2016 .

[2]  Xiaodong Wang,et al.  Flutter analysis of bending–torsion coupling of aero-engine compressor blade with assembled clearance , 2015 .

[3]  Yushu Chen,et al.  Influencing factors of the dynamic hysteresis in varying compliance vibrations of a ball bearing , 2015 .

[4]  Zhifeng Hao,et al.  The isolation characteristics of an archetypal dynamical model with stable-quasi-zero-stiffness , 2015 .

[5]  Yueming Li,et al.  Efficient aero-structural design optimization: Coupling based on reverse iteration of structural model , 2015 .

[6]  Yiren Yang,et al.  Nonlinear flutter behavior of a plate with motion constraints in subsonic flow , 2014 .

[7]  Feixin Chen,et al.  Calculations of the bounds on limit cycle oscillations in nonlinear aeroelastic systems based on equivalent linearization , 2014 .

[8]  L. Li,et al.  Flapwise non-linear dynamics of wind turbine blades with both external and internal resonances , 2014 .

[9]  Wei Zhang,et al.  Validation of dynamic cavitation model for unsteady cavitating flow on NACA66 , 2014 .

[10]  Jinchen Ji,et al.  Design of a nonlinear vibration absorber using three-to-one internal resonances , 2014 .

[11]  Cyril Touzé,et al.  Nonlinear forced vibrations of thin structures with tuned eigenfrequencies: the cases of 1:2:4 and 1:2:2 internal resonances , 2014 .

[12]  L. Hou,et al.  Analysis of 1/2 sub-harmonic resonance in a maneuvering rotor system , 2013, Science China Technological Sciences.

[13]  Yukio Ishida,et al.  Flow‐Induced Vibrations , 2012 .

[14]  Yushu Chen,et al.  Supercritical and subcritical Hopf bifurcation and limit cycle oscillations of an airfoil with cubic nonlinearity in supersonic\hypersonic flow , 2012 .

[15]  Na Zhao,et al.  Active control of supersonic/hypersonic aeroelastic flutter for a two-dimensional airfoil with flap , 2011 .

[16]  Liangqiang Zhou,et al.  Bifurcation and chaos of an airfoil with cubic nonlinearity in incompressible flow , 2011 .

[17]  M. A. Barron-Meza Vibration Analysis Of a Self-Excited Elastic Beam , 2010 .

[18]  Mihir Sen,et al.  Synchronization of coupled self-excited elastic beams , 2009 .

[19]  M. Wiercigroch,et al.  A Reduced Order Model for Vortex–Induced Vibration of a Vertical Offshore Riser in Lock–in , 2008 .

[20]  Fumio Inada,et al.  Flow Induced Vibrations : Classifications and Lessons from Practical Experiences , 2008 .

[21]  D. Simoni,et al.  Von Karman Vortices Formation at the Trailing Edge of a Turbine Blade , 2008 .

[22]  Randolph C. K. Leung,et al.  Vortex-induced vibration effect on fatigue life estimate of turbine blades , 2007 .

[23]  Kwok-Wai Chung,et al.  Bifurcation analysis of a two-degree-of-freedom aeroelastic system with hysteresis structural nonlinearity by a perturbation-incremental method , 2007 .

[24]  Alexander F. Vakakis,et al.  Suppression of limit cycle oscillations in the van der Pol oscillator by means of passive non‐linear energy sinks , 2006 .

[25]  Max F. Platzer,et al.  On Vortex Formation in the Wake Flows of Transonic Turbine Blades and Oscillating Airfoils , 2006 .

[26]  Haym Benaroya,et al.  An overview of modeling and experiments of vortex-induced vibration of circular cylinders , 2005 .

[27]  John Young,et al.  Oscillation Frequency and Amplitude Effects on the Wake of a Plunging Airfoil , 2004 .

[28]  Randolph C. K. Leung,et al.  Aerodynamic and Structural Resonance of an Elastic Airfoil Due to Oncoming Vortices , 2004 .

[29]  E. de Langre,et al.  Coupling of Structure and Wake Oscillators in Vortex-Induced Vibrations , 2004 .

[30]  C. H. Sieverding,et al.  Turbine Blade Trailing Edge Flow Characteristics at High Subsonic Outlet Mach Number , 2003 .

[31]  C. H. Sieverding,et al.  Unsteady Turbine Blade Wake Characteristics , 2003 .

[32]  S. J. Price,et al.  NONLINEAR AEROELASTIC ANALYSIS OF AIRFOILS : BIFURCATION AND CHAOS , 1999 .

[33]  Pascal Hémon,et al.  AN IMPROVEMENT OF THE TIME DELAYED QUASI-STEADY MODEL FOR THE OSCILLATIONS OF CIRCULAR CYLINDERS IN CROSS-FLOW , 1999 .

[34]  Søren Nielsen,et al.  Energy Balanced Double Oscillator Model for Vortex-Induced Vibrations , 1999 .

[35]  Marina Ubaldi,et al.  An experimental study of the unsteady characteristics of the turbulent wake of a turbine blade , 1999 .

[36]  C. M. Dohring,et al.  Experimental and Computational Investigation of the Knoller-Betz Effect , 1998 .

[37]  Stuart J. Price,et al.  The post-Hopf-bifurcation response of an airfoil in incompressible two-dimensional flow , 1996 .

[38]  C. H. Sieverding,et al.  The Effect of Vortex Shedding on the Unsteady Pressure Distribution Around the Trailing Edge of a Turbine Blade , 1996 .

[39]  B. R. Noack,et al.  On cell formation in vortex streets , 1991, Journal of Fluid Mechanics.

[40]  Earl H. Dowell,et al.  Comparison of Theory and Experiment for Nonlinear Flutter and Stall Response of Helicopter Blade , 1991 .

[41]  O. M. Griffin,et al.  A model for the vortex-excited resonant response of bluff cylinders , 1973 .

[42]  Hideo Ohashi,et al.  Visualization Study of Flow Near the Trailing Edge of an Oscillating Airfoil , 1972 .

[43]  I. G. Currie,et al.  Lift-Oscillator Model of Vortex-Induced Vibration , 1970 .

[44]  Richard Evelyn Donohue Bishop,et al.  The lift and drag forces on a circular cylinder in a flowing fluid , 1964, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[45]  Yuan-Cheng Fung,et al.  An introduction to the theory of aeroelasticity , 1955 .

[46]  C. Chan,et al.  Bifurcation analysis of a two-degree-of-freedom aeroelastic system with freeplay structural non-linearity by a perturbation-incremental method , 2022 .