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-  2018 

复合材料梁的几何精确非线性建模及非经典效应
Geometrically exact nonlinear modeling and non-classical effect influence of composite beams

DOI: 10.13801/j.cnki.fhclxb.20170412.003

Keywords: 复合材料梁,几何精确,非经典效应,翘曲,横向剪切变形
composite beam
,geometrically exact,non-classical effect,warping,transverse shear deformation

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[1]  HONG C H, CHOPRA I. Aeroelastic stability analysis of a composite rotor blade[J]. Journal of the American Helicopter Society, 1985, 30(2):57-67.
[2]  SMITH E C, CHOPRA I. Formulation and evaluation of an analytical model for composite box-beams[J]. Journal of the American Helicopter Society, 1990, 36(3):23-35.
[3]  SMITH E C, CHOPRA I. Aeroelastic response, loads and stability of a composite rotor in forward flight[J]. AIAA Journal, 1993, 31(7):1265-1273.
[4]  SMITH E C, CHOPRA I. Air and ground resonance of helicopters with elastically tailored composite rotor blades[J]. Journal of the American Helicopter Society, 1993, 38(4):50-61.
[5]  JUNG S N, NAGARAJ V T, CHOPRA I. Refined structural model for thin and thick-walled composite rotor blades[J]. AIAA Journal, 2002, 40(1):105-116.
[6]  HODGES D H. A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams[J]. International Journal of Solids and Structures, 1990, 26(11):1253-1273.
[7]  HODGES D H. Nonlinear composite beam theory[M]. Reston:AIAA, 2006.
[8]  YU W. Efficient high-fidelity simulation of multibody systems with composite dimensionally reducible components[J]. Journal of the American Helicopter Society, 2007, 52(1):49-57.
[9]  HO J C, YU W, HODGES D H. Energy transformation to generalized Timoshenko form by the variational asymptotic beam sectional analysis[C]//51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Orlando:American Institute of Aeronautics and Astronautics, 2010.
[10]  YU W, BLAIR M. GEBT:A general-purpose nonlinear analysis tool for composite beams[J]. Composite Structures, 2012, 94(9):2677-2689.
[11]  YUAN K A, FRIEDMANN P P, VENKATESAN C. A new aeroelastic model for composite rotor blades with straight and swept tips[C]//33rd AIAA/AHS/ASME/ASCE/ASC Structures, Structural Dynamics and Materials Conference. Dallas:American Institute of Aeronautics and Astronautics, 1992.
[12]  YUAN K A, FRIEDMANN P P, VENKATESAN C. Aeroelastic stability response and loads of swept tip composite rotor blades in forward flight[C]//35th AIAA/AHS/ASME/ASCE/ASC Structures, Structural Dynamics and Materials Conference. Hilton Head:American Institute of Aeronautics and Astronautics, 1994.
[13]  尹维龙, 向锦武. 弹性耦合对直升机复合材料桨叶稳定性的影响[J]. 复合材料学报, 2006, 23(4):143-148. YIN W L, XIANG J W. Stability analysis for helicopter composite rotor blades with elastic coupling[J]. Acta Materiae Compositae Sinica, 2006, 23(4):143-148.
[14]  尹维龙, 向锦武. 考虑剪切和翘曲影响的直升机旋翼气弹稳定性分析[J]. 航空学报, 2006, 27(6):1130-1134. YIN W L, XIANG J W. Aeroelastic stability for helicopter rotor blades with consideration of transverse shear deformation and warping[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(6):1130-1134.
[15]  尹维龙, 向锦武. 弹性耦合对复合材料旋翼前飞气弹响应及载荷的影响[J]. 航空学报, 2007, 28(3):605-609. YIN W L, XIANG J W. Aeroelastic response and hub load of composite hingeless rotor in forward flight with elastic couplings[J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(3):605-609.
[16]  FRIEDMANN P, GLAZ B, PALACIOS P. A moderate deflection composite helicopter rotor blade model with an improved cross-sectional analysis[J]. International Journal of Solids and Structures, 2008, 46(10):2186-2200.
[17]  CHANDRA R, STEMPLE D A, CHOPRA I. Thin-walled composite beams under bending, torsional and extensional loads[J]. Journal of Aircraft, 1990, 27(7):619-626.
[18]  CHANDRA R, CHOPRA I. Experimental-theorectical investigation of the vibration characteristics of rotating composite box beams[J]. Journal of Aircraft, 1992, 29(4):657-664.
[19]  HODGES D H, DOWELL E H. Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades, NASA-TN-D-7818[R]. Washington:NASA, 1974.
[20]  MEGSON T H G. Linear analysis of thin-walled elastic structures[M]. New York:John Wiley & Sons, 1974.
[21]  DANIELSON D A, HODGES D H. Nonlinear beam kinematics by decomposition of the rotation tensor[J]. Journal of Applied Mechanics, 1987, 54(2):258-262.
[22]  JUNG S N, NAGARAJ V T, CHOPRA I. Refined structural dynamics model for composite rotor blades[J]. AIAA Journal, 2001, 39(2):339-348.

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