Rotor Loads Prediction Utilizing a Coupled Aeroelastic Analysis with Refined Aerodynamic Modeling

[1]  D. Peters,et al.  Effectiveness of Current Dynamic-Inflow Models in Hover and Forward Flight , 1986 .

[2]  Ruth M. Heffernan,et al.  AIAA-87-0919-CP Effect of Helicopter Blade Dynamics on Blade Aerodynamic and Structural Loads , 1988 .

[3]  R. M. Heffernan,et al.  Structural and aerodynamic loads and performance measurements of an SA349/2 helicopter with an advanced geometry rotor , 1986 .

[4]  Peretz P. Friedmann,et al.  A new look at arbitrary motion unsteady aerodynamics and its application to rotary-wing aeroelasticity , 1985 .

[5]  Inderjit Chopra,et al.  Flap-Lag-Torsion Stability in Forward Flight , 1985 .

[6]  S. T. Gangwani.  Synthesized airfoil data method for prediction of dynamic stall and unsteady airloads , 1983 .

[7]  Inderjit Chopra,et al.  Response and hub loads sensitivity analysis of a helicopter rotor , 1990 .

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

[9]  Wayne Johnson,et al.  A Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics. Part 1. Analysis Development , 1980 .

[10]  Khanh Nguyen,et al.  APPLICATION OF HIGHER HARMONIC CONTROL (HHC) TO HINGELESS ROTOR SYSTEMS , 1989 .

[11]  J. G. Leishman,et al.  A Semi-Empirical Model for Dynamic Stall , 1989 .

[12]  F. X. Caradonna,et al.  A review of current finite difference rotor flow methods , 1986 .

[13]  Peretz P. Friedmann,et al.  Application of time-domain unsteady aerodynamics to rotary-wing aeroelasticity , 1986 .

[14]  Anton J. Landgrebe,et al.  The Wake Geometry of a Hovering Helicopter Rotor and its Influence on Rotor Performance , 1972 .

[15]  Gloria K. Yamauchi,et al.  Correlation of SA349/2 helicopter flight-test data with a comprehensive rotorcraft model , 1988 .