Lagrangian formulation for the rapid estimation of helicopter rotor blade vibration characteristics
暂无分享,去创建一个
[1] Olivier A. Bauchau,et al. Nonlinear Composite Beam Theory , 1988 .
[2] Roberto Celi,et al. High-order state space simulation models of helicopter flight mechanics , 1993 .
[3] V. R. Murthy,et al. Dynamic characteristics of rotor blades , 1976 .
[4] Olivier A. Bauchau,et al. Finite Element Approach to Rotor Blade Modeling , 1987 .
[5] Alessandro Fasana,et al. RAYLEIGH-RITZ ANALYSIS OF SANDWICH BEAMS , 2001 .
[6] Cristinel Mares,et al. COUPLED BENDING–BENDING–TORSION VIBRATION ANALYSIS OF ROTATING PRETWISTED BLADES: AN INTEGRAL FORMULATION AND NUMERICAL EXAMPLES , 1997 .
[7] E. Wilde,et al. A Theoretical Method for Calculating Flexure and Stresses in Helicopter Rotor Blades , 1965 .
[8] V. R. Murthy,et al. Dynamic characteristics of stiffened rings by transfer matrix approach , 1975 .
[9] Dewey H. Hodges,et al. Vibration and Response of Nonuniform Rotating Beams with Discontinuities , 1979 .
[10] David A. Peters,et al. Finite-State Induced-Flow Model for Rotors in Hover and Forward Flight , 1989 .
[11] Roberto Celi,et al. Coupled Rotor-Fuselage Dynamics and Aeroelasticity in Turning Flight , 1995 .
[12] Olivier A. Bauchau,et al. Structural dynamics of a helicopter rotor blade system , 1988 .
[13] Roberto Celi,et al. Forward flight trim and frequency response validation of a helicopter simulation model , 1993 .