Implications of warping restraint on statics and dynamics of elastically tailored thin-walled composite beams
暂无分享,去创建一个
[1] Ohseop Song,et al. On the static aeroelastic tailoring of composite aircraft swept wings modelled as thin-walled beam structures☆ , 1992 .
[2] Chyanbin Hwu,et al. Aeroelastic Divergence of Stiffened Composite Multicell Wing Structures , 2002 .
[3] Scott R. White,et al. Thick-walled composite beam theory including 3-d elastic effects and torsional warping , 1997 .
[4] Anthony N. Palazotto,et al. Vibration and buckling characteristics of composite cylindrical panels incorporating the effects of a higher order shear theory , 1991 .
[5] A. Gjelsvik,et al. The Theory of Thin-Walled Bars , 1981 .
[6] Inderjit Chopra,et al. Assessment of Composite Rotor Blade Modeling Techniques , 1999 .
[7] T. A. Weisshaar,et al. Aeroelastic tailoring - Theory, practice, and promise , 1984 .
[8] Liviu Librescu,et al. Aeroelastic instability and response of advanced aircraft wings at subsonic flight speeds , 2002 .
[9] L. Librescu,et al. General formulation for the aeroelastic divergence of composite swept-forward wing structures , 1988 .
[10] Ohseop Song,et al. Behavior of Thin-Walled Beams Made of Advanced Composite Materials and Incorporating Non-Classical Effects , 1991 .
[11] Leonard Meirovitch,et al. Control of Cantilever Vibration via Structural Tailoring and Adaptive Materials , 1997 .
[12] Liviu Librescu,et al. Free Vibration Of Anisotropic Composite Thin-Walled Beams Of Closed Cross-Section Contour , 1993 .
[13] Ohseop Song,et al. Modeling and response analysis of thin-walled beam structures constructed of advanced composite materials , 1990 .