Nonlinear Reduced-Order Models for Transonic Aeroelastic and Aeroservoelastic Problems

Nonlinear reduced-order modeling approaches have been a promising tool for predicting the transonic aerodynamic and aeroelastic behaviors of aircraft structures. However, the accuracy of the approa...

[1]  Oddvar O. Bendiksen Transonic Limit Cycle Flutter of High-Aspect-Ratio Swept Wings , 2008 .

[2]  Bart De Moor,et al.  Combined Deterministic-Stochastic Identification , 1996 .

[3]  Haiyan Hu,et al.  Nonlinear Reduced-Order Modeling for Multiple-Input/Multiple-Output Aerodynamic Systems , 2014 .

[4]  Walter A. Silva,et al.  Application of nonlinear systems theory to transonic unsteady aerodynamic responses , 1993 .

[5]  Earl H. Dowell,et al.  Reduced-Order Models for Computational-Fluid-Dynamics-Based Nonlinear Aeroelastic Problems , 2015 .

[6]  R Waszak Martin,et al.  Modeling the Benchmark Active Control Technology Wind-Tunnel Model for Application to Flutter Suppression , 1996 .

[7]  Walter A. Silva,et al.  Development of Reduced-Order Models for Aeroelastic Analysis and Flutter Prediction Using the CFL3Dv6.0 Code , 2002 .

[8]  Taehyoun Kim,et al.  Parametric model reduction for aeroelastic systems: Invariant aeroelastic modes , 2016 .

[9]  Jeffrey P. Thomas,et al.  Computation of Unsteady Nonlinear Flows in Cascades Using a Harmonic Balance Technique , 2002 .

[10]  Earl H. Dowell,et al.  Reduced-Order Modeling of Flutter and Limit-Cycle Oscillations Using the Sparse Volterra Series , 2012 .

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

[12]  Bryan Glaz,et al.  Reduced-Order Nonlinear Unsteady Aerodynamic Modeling Using a Surrogate-Based Recurrence Framework , 2010 .

[13]  Haiyan Hu,et al.  Open/Closed-Loop Aeroservoelastic Predictions via Nonlinear, Reduced-Order Aerodynamic Models , 2015 .

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

[15]  Sergio Ricci,et al.  Active Aeroelastic Control Over a Multisurface Wing: Modeling and Wind-Tunnel Testing , 2007 .

[16]  Carlos E. S. Cesnik,et al.  Reduced-Order Aerothermoelastic Framework for Hypersonic Vehicle Control Simulation , 2010 .

[17]  W. Rodden,et al.  A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows. , 1969 .

[18]  Haiyan Hu,et al.  Wind-Tunnel Tests for Active Flutter Control and Closed-Loop Flutter Identification , 2016 .

[19]  Simao Marques,et al.  Prediction of Transonic Limit-Cycle Oscillations Using an Aeroelastic Harmonic Balance Method , 2015 .

[20]  Haiyan Hu,et al.  Efficient reduced-order modeling of unsteady aerodynamics robust to flight parameter variations , 2014 .

[21]  Vivek Mukhopadhyay,et al.  Flutter suppression control law design and testing for the active flexible wing , 1995 .

[22]  Christian Breitsamter,et al.  Neurofuzzy-Model-Based Unsteady Aerodynamic Computations Across Varying Freestream Conditions , 2016 .

[23]  Vivek Mukhopadhyay,et al.  Transonic Flutter Suppression Control Law Design and Wind-Tunnel Test Results , 2000 .

[24]  Qiang Zhou,et al.  Computational fluid dynamics-based transonic flutter suppression with control delay , 2016 .

[25]  Jeffrey P. Thomas,et al.  Proper Orthogonal Decomposition Technique for Transonic Unsteady Aerodynamic Flows , 2000 .

[26]  R Waszak Martin,et al.  Robust Multivariable Flutter Suppression for the Benchmark Active Control Technology (BACT) Wind-tunnel Model , 1997 .

[27]  Earl H. Dowell,et al.  Proper Orthogonal Decomposition Reduced-Order Model for Nonlinear Aeroelastic Oscillations , 2014 .

[28]  K. Isogai,et al.  Transonic dip mechanism of flutter of a sweptback wing. II , 1981 .