Efficient Method for Limit Cycle Flutter Analysis Based on Nonlinear Aerodynamic Reduced-Order Models

[1]  Bryan Glaz,et al.  A surrogate based approach to reduced-order dynamic stall modeling , 2010 .

[2]  Weiwei Zhang,et al.  Effect of control surface on airfoil flutter in transonic flow , 2010 .

[3]  Jeffrey P. Thomas,et al.  Using Automatic Differentiation to Create a Nonlinear Reduced-Order-Model Aerodynamic Solver , 2010 .

[4]  Fred Nitzsche,et al.  Application of Multi-Input Volterra Theory to Nonlinear Multi-Degree-of-Freedom Aerodynamic Systems , 2010 .

[5]  Weiwei Zhang,et al.  Aeroservoelastic Analysis for Transonic Missile Based on Computational Fluid Dynamics , 2009 .

[6]  Qing Yang,et al.  Gust Response Analysis Using CFD-Based Reduced Order Models , 2009 .

[7]  Martin D. Buhmann,et al.  Radial Basis Functions: Theory and Implementations: Preface , 2003 .

[8]  Zhang Weiwei ON UNSTEADY AERODYNAMIC MODELING BASED ON CFD TECHNIQUE AND ITS APPLICATIONS ON AEROELASTIC ANALYSIS , 2008 .

[9]  Weiwei Zhang,et al.  Reduced-Order-Model-Based Flutter Analysis at High Angle of Attack , 2007 .

[10]  Jonathan E. Cooper,et al.  Bifurcation analysis and limit cycle oscillation amplitude prediction methods applied to the aeroelastic galloping problem , 2007 .

[11]  Weiwei Zhang,et al.  ROM Based Aeroservoelastic Analysis in Transonic Flow , 2007 .

[12]  Ken Badcock,et al.  Non-linear aeroelastic prediction for aircraft applications , 2007 .

[13]  Oddvar O. Bendiksen,et al.  High-Altitude Limit Cycle Flutter of Transonic Wings , 2007 .

[14]  Weiwei Zhang,et al.  Control law design for transonic aeroservoelasticity , 2007 .

[15]  Weiwei Zhang,et al.  Two Better Loosely Coupled Solution Algorithms of CFD Based Aeroelastic Simulation , 2007 .

[16]  Philip S. Beran,et al.  Computational Aeroelastic Analysis of Store-Induced Limit-Cycle Oscillation , 2007 .

[17]  Oddvar O. Bendiksen,et al.  Transonic Limit Cycle Flutter of High-Aspect-Ratio Swept Wings , 2006 .

[18]  Feng Liu,et al.  Prediction of Flutter and LCO by an Euler Method on Non-moving Cartesian Grids with Boundary-Layer Corrections , 2005 .

[19]  W. Silva,et al.  Identification of Nonlinear Aeroelastic Systems Based on the Volterra Theory: Progress and Opportunities , 2005 .

[20]  David J. Lucia,et al.  Reduced-order modelling of limit-cycle oscillation for aeroelastic systems , 2004 .

[21]  Earl H. Dowell,et al.  Modeling the LCO of a Delta Wing Using a High , 2004 .

[22]  Liviu Librescu,et al.  Nonlinear Open-/Closed-Loop Aeroelastic Analysis of Airfoils via Volterra Series , 2004 .

[23]  P. Beran,et al.  Reduced-order modeling: new approaches for computational physics , 2004 .

[24]  Ann L Gaitonde,et al.  Identification of limit cycles for piecewise nonlinear aeroelastic systems , 2002 .

[25]  Liviu Librescu,et al.  Open/Closed-Loop Nonlinear Aeroelasticity for Airfoils via Volterra Series Approach , 2002 .

[26]  Jeffrey P. Thomas,et al.  Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter, and Limit-Cycle Oscillations , 2001 .

[27]  Carlos E. S. Cesnik,et al.  Limit-cycle oscillations in high-aspect-ratio wings , 2002 .

[28]  Jeffrey P. Thomas,et al.  Transonic Limit Cycle Oscillation Analysis Using Reduced Order Aerodynamic Models , 2001 .

[29]  Daniella E. Raveh,et al.  Reduced-Order Models for Nonlinear Unsteady Aerodynamics , 2001 .

[30]  Earl H. Dowell,et al.  Modeling of Fluid-Structure Interaction , 2001 .

[31]  Earl H. Dowell,et al.  Experimental and Theoretical Study on Aeroelastic Response of High-Aspect-Ratio Wings , 2001 .

[32]  F. Marques,et al.  IDENTIFICATION AND PREDICTION OF UNSTEADY TRANSONIC AERODYNAMIC LOADS BY MULTI-LAYER FUNCTIONALS , 2001 .

[33]  N. Sundararajan,et al.  Radial Basis Function Neural Networks with Sequential Learning , 1999 .

[34]  Earl H. Dowell,et al.  LIMIT CYCLE OSCILLATIONS OF DELTA WING MODELS IN LOW SUBSONIC FLOW , 1999 .

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

[36]  Simon Haykin,et al.  Neural Networks: A Comprehensive Foundation , 1998 .

[37]  William E. Faller,et al.  Unsteady fluid mechanics applications of neural networks , 1995 .

[38]  Robert M. Bennett,et al.  NACA 0012 benchmark model experimental flutter results with unsteady pressure distributions , 1992 .