scholarly journals Free vibration of axially loaded thin-walled composite Timoshenko beams

2010 ◽  
Vol 81 (9) ◽  
pp. 1165-1180 ◽  
Author(s):  
Thuc Phuong Vo ◽  
Jaehong Lee
2004 ◽  
Vol 46 (2) ◽  
pp. 299-320 ◽  
Author(s):  
Jun Li ◽  
Rongying Shen ◽  
Hongxing Hua ◽  
Xianding Jin

2009 ◽  
Vol 90 (2) ◽  
pp. 233-241 ◽  
Author(s):  
Thuc Phuong Vo ◽  
Jaehong Lee

2010 ◽  
Vol 48 (12) ◽  
pp. 915-920 ◽  
Author(s):  
Fernanda de Borbón ◽  
Daniel Ambrosini

1999 ◽  
Author(s):  
Sungsoo Na ◽  
Liviu Librescu

Abstract A study of the dynamical behavior of aircraft wings modeled as doubly-tapered thin-walled beams, made from advanced anisotropic composite materials, and incorporating a number of non-classical effects such as transverse shear, and warping inhibition is presented. The supplied numerical results illustrate the effects played by the taper ratio, anisotropy of constituent materials, transverse shear flexibility, and warping inhibition on free vibration and dynamic response to time-dependent external excitations. Although considered for aircraft wings, this analysis and results can be also applied to a large number of structures such as helicopter blades, robotic manipulator arms, space booms, tall cantilever chimneys, etc.


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