The SHARCS project: Smart hybrid active rotor control system for noise and vibration attenuation of helicopter rotor blades
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Giuliano Coppotelli | Gian Luca Ghiringhelli | Massimo Gennaretti | Fred Nitzsche | Daniel Feszty | D. Waechter | E. Bianchi | S. Voutsinas | M. Gennaretti | G. Coppotelli | E. Bianchi | G. Ghiringhelli | F. Nitzsche | D. Waechter | D. Feszty | S. Voutsinas
[1] J Mayo Greenberg,et al. Airfoil in sinusoidal motion in a pulsating stream , 1947 .
[2] Massimo Gennaretti,et al. Aeroelastic Modeling and Vibratory Load Analysis of Helicopters , 2004 .
[3] T. Aoyama. Calculation of Rotor Blade-Vortex Interaction Noise using Parallel Super Computer , 1996 .
[4] Giuliano Coppotelli,et al. Output-Only Approach for Finite Element Model Updating of AB-204 Helicopter Blade , 2005 .
[5] Palle Andersen,et al. Modal Identification from Ambient Responses using Frequency Domain Decomposition , 2000 .
[6] Rune Brincker,et al. Why Output-Only Modal Testing is a Desirable Tool for a Wide Range of Practical Applications , 2002 .
[7] Rune Brincker,et al. On Modal Parameter Estimates from Ambient Vibration Tests , 2004 .
[8] Jianhua Zhang,et al. Active-Passive Hybrid Optimization of Rotor Blades With Trailing Edge Flaps , 2000 .
[9] Viresh Wickramasinghe,et al. Development of a Maximum Energy Extraction Control for the Smart Spring , 2005 .
[10] B. Richards,et al. Elements of computational fluid dynamics on block structured grids using implicit solvers , 2000 .
[11] Fred Nitzsche,et al. Acoustic validation of a new code using particle wake aerodynamics and geometrically-exact beam structural dynamics , 2005, The Aeronautical Journal (1968).
[12] T. Theodorsen. General Theory of Aerodynamic Instability and the Mechanism of Flutter , 1934 .
[13] Fred Nitzsche,et al. Trailing edge flow control for the mitigation of dynamic stall effects , 2005 .
[14] Farhan Gandhi,et al. Helicopter Vibration Reduction Using Discrete Controllable-Stiffness Devices at the Rotor Hub , 2001 .
[15] Earl H. Dowell,et al. Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades , 1974 .
[16] Friedrich K. Straub,et al. Design and testing of a double X-frame piezoelectric actuator , 2000, Smart Structures.
[17] E. A. Gillies,et al. Alleviation of Airfoil Dynamic Stall Moments via Trailing-Edge-Flap Flow Control , 2004 .
[18] Paolo Mantegazza,et al. Analysis of an actively twisted rotor by multibody global modeling , 2001 .
[19] Carlos E. Ventura,et al. Why Output Only Modal Analysis is a Desirable Tool for a Wide Range of Practical Applications , 2003 .
[20] D. H. Roberta. Hodges,et al. Stability of elastic bending and torsion of uniform cantilever rotor blades in hover with variable structural coupling , 1976 .
[21] W. R. Splettstoesser,et al. The HELINOISE Aeroacoustic Rotor Test in the DNW , 1993 .
[22] Vincent Hayward,et al. Single state elastoplastic friction models , 2002, IEEE Trans. Autom. Control..
[23] Carlos Canudas de Wit,et al. A survey of models, analysis tools and compensation methods for the control of machines with friction , 1994, Autom..