Periodic Response of Thin-Walled Composite Helicopter Rotor Blades
暂无分享,去创建一个
[1] Omri Rand,et al. Influence of Interactional Aerodynamics on Helicopter Rotor/Fuselage Coupled Response in Hover and Forward Flight , 1989 .
[2] John Dugundji,et al. Experiments and analysis for composite blades under large deflections. II - Dynamic behavior , 1990 .
[3] Alan D. Stemple,et al. Finite-Element Model for Composite Beams with Arbitrary Cross-Sectional Warping , 1988 .
[4] O. Bauchau. A Beam Theory for Anisotropic Materials , 1985 .
[5] Olivier A. Bauchau,et al. Large displacement analysis of naturally curved and twisted composite beams , 1987 .
[6] Inderjit Chopra,et al. Aeroelastic Stability Analysis of a Composite Rotor Blade , 1985 .
[7] Inderjit Chopra,et al. Aeroelastic Stability Analysis of a Composite Bearingless Rotor Blade , 1986 .
[8] Alan D. Stemple,et al. A finite element model for composite beams undergoing large deflection with arbitrary cross‐sectional warping , 1989 .
[9] Peretz P. Friedmann,et al. Helicopter rotor dynamics and aeroelasticity - Some key ideas and insights , 1990 .
[10] Peretz P. Friedmann,et al. Vibration analysis of composite turbopropellers using a nonlinear beam-type finite-element approach , 1989 .