Structural response of composite beams and blades with elastic couplings

Composites Engineering - Tập 2 - Trang 347-374 - 1992
Ramesh Chandra1, Inderjit Chopra1
1Center for Rotorcraft Education and Research, Department of Aerospace Engineering, University of Maryland, College Park, MD 20742, U.S.A.

Tài liệu tham khảo

Bauchau, 1987, Large displacement analysis of naturally curved and twisted composite beams, AIAA Jl, 25, 1469, 10.2514/3.9806 Borri, 1986, A large displacement formulation for anisotropic beam analysis, Meccanica, 21, 30, 10.1007/BF01556314 Chandra, 1991, Experimental and theoretical analysis of composite I-beams with elastic couplings, AIAA Jl, 29, 2197, 10.2514/3.10860 Chandra, 1991, Vibration characteristics of composite I-beams with elastic couplings under rotation Chandra, 1991, Structural behavior of two-cell composite rotor blades with elastic couplings Chandra, 1991, Coupled composite rotor blades under bending and torsional loads Chandra, 1992, Experimental-theoretical investigation of the vibration characteristics of rotating composite box beams, J. Aircraft, 10.2514/3.46216 Chandra, 1990, Thin-walled composite beams under bending, torsional and extensional loads, J. Aircraft, 27, 619, 10.2514/3.25331 Giavotto, 1983, Anisotropic beam theory and application, Comput. Struct, 16, 403, 10.1016/0045-7949(83)90179-7 Gjelsvik, 1981 Hodges, 1991, Free-vibration analysis of composite beams, J. Am. Helicopter Soc, 36, 36, 10.4050/JAHS.36.36 Hodges, 1974, Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades, NASA TN D-7818 Hong, 1985, Aeroelastic stability of a composite blade, J. Am. Helicopter Soc, 30, 57, 10.4050/JAHS.30.57 Kosmatka, 1991, Extension-bend-twist coupling behavior of thin-walled advanced composite beams with initial twist Megson, 1974 Minguet, 1990, Experiments and analysis for composite blades under large deflections, Part 1: Static behavior, AIAA Jl, 28, 1573, 10.2514/3.25255 Minguet, 1990, Experiments and analysis for composite blades under large deflections, Part 2: Dynamic behavior, AIAA Jl, 28, 1580, 10.2514/3.25256 Nixon, 1987, Extension-twist coupling of composite circular tubes with application to tilt rotor blade design Rehfield, 1989, On the buckling behavior of thin walled laminated composite open section beams Rehfield, 1988, Structural modeling for multicell composite rotor blades Rehfield, 1990, Nonclassical behavior of thin-walled composite beams with closed cross-sections, J. Am. Helicopter Soc, 35, 42, 10.4050/JAHS.35.42 Smith, 1991, Formulation and evaluation of an analytical model for composite box beams, J. Am. Helicopter Soc, 36, 23, 10.4050/JAHS.36.23 Vlasov, 1961