Validation of Structural and Aerodynamic Modeling Using UH-60A Airloads Program Data

[1]  John Vorwald,et al.  Dynamics Workshop On Rotor Vibratory Loads Prediction , 1998 .

[2]  William G. Bousman,et al.  Technical Note: A Note on Torsional Dynamic Scaling , 1998 .

[3]  Baeder,et al.  Validation of UH-60A Rotor Blade Aerodynamic Characteristics Using CFD , 2003 .

[4]  Wayne Johnson,et al.  Rotorcraft Aerodynamics Models for a Comprehensive Analysis , 1998 .

[5]  William G. Bousman,et al.  Putting the Aero Back into Aeroelasticity , 1999 .

[6]  J. Leishman Validation of approximate indicial aerodynamic functions for two-dimensional subsonic flow , 1988 .

[7]  J. Gordon Leishman,et al.  Rotor Free-Wake Modeling Using a Pseudo-Implicit Technique — Including Comparisons with Experimental Data , 1995 .

[8]  William G. Bousman,et al.  The response of helicopter rotors to vibratory airload , 1990 .

[9]  Inderjit Chopra,et al.  Aeroelastic optimization of an advanced geometry helicopter rotor , 1992 .

[10]  James D. Baeder,et al.  Indicial Aerodynamics in Compressible Flow-Direct Computational Fluid Dynamic Calculations , 1997 .

[11]  Joon W. Lim,et al.  Correlation of 2GCHAS Analysis with Experimental Data , 1995 .

[12]  James D. Baeder,et al.  Field Velocity Approach and Geometric Conservation Law for Unsteady Flow Simulations , 2003 .

[13]  W. Johnson,et al.  Wake model for helicopter rotors in high speed flight , 1988 .

[14]  Hubert Pomin,et al.  Aeroelastic Analysis of Helicopter Rotor Blades on Deformable Chimera Grids , 2004 .

[15]  William G. Bousman,et al.  Technical Note: UH-60A Airloads Program Azimuth Reference Correction , 2005 .

[16]  R. Barron On Newtonian flow past power-law bodies , 1977 .

[17]  Anubhav Datta,et al.  Validation and Understanding of UH-60A Vibratory Loads in Steady Level Flight , 2002 .

[18]  Mark Potsdam,et al.  Rotor Airloads Prediction Using Loose Aerodynamic/Structural Coupling , 2004 .

[19]  Michael S. Torok,et al.  Aerodynamic and Wake Methodology Evaluation Using Model UH-60A Experimental Data , 1994 .

[20]  Carl Albrecht Transmission Design Using Finite Element Method Analysis Techniques , 1988 .

[21]  Altmikus,et al.  A Comparison: Weak Versus Strong Modular Coupling for Trimmed Aeroelastic Rotor Simulations , 2002 .

[22]  David A. Peters,et al.  On the nonlinear deformation geometry of Euler-Bernoulli beams. [rotary wings] , 1980 .

[23]  K. R. V. Kaza,et al.  Nonlinear Curvature Expressions for Combined Flapwise Bending, Chordwise Bending, Torsion and Extension of Twisted Rotor Blades , 1976 .

[24]  J. Baeder,et al.  Flowfield of a Lifting Rotor in Hover: A Navier-Stokes Simulation , 1992 .

[25]  Michael S. Torok,et al.  Analysis of Rotor Blade Dynamics Using Model Scale UH-60A Airloads , 1994 .

[26]  William G. Bousman,et al.  Calculated and Measured Blade Structural Response on a Full-Scale Rotor , 1986 .

[27]  Earl H. Dowell,et al.  Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades , 1974 .

[28]  Wayne Johnson,et al.  The Effects of Control System Stiffness Models on the Dynamic Stall Behavior of a Helicopter , 2000 .

[29]  Peter F. Lorber,et al.  Aerodynamic Results of a Pressure-Instrumented Model Rotor Test at the DNW , 1991 .

[30]  J. Baeder,et al.  TURNS - A free-wake Euler/Navier-Stokes numerical method for helicopter rotors , 1993 .

[31]  P. Goorjian,et al.  Computation of Unsteady Transonic Flows by the Indicial Method , 1977 .