Inclusion of transverse shear deformation in optimum design of aircraft wing panels

1996 ◽  
Author(s):  
P. Williams ◽  
F. Williams ◽  
D. Kennedy
Keyword(s):  
Shear Deformation ◽  
Optimum Design ◽  
Transverse Shear ◽  
Transverse Shear Deformation ◽  
Aircraft Wing

Inclusion of transverse shear deformation in optimum design of aircraft wing panels

AIAA Journal ◽  
1996 ◽  
Vol 34 (11) ◽  
pp. 2456-2458 ◽  
Author(s):  
Phil W. L. Williams ◽  
Fred W. Williams ◽  
David Kennedy
Keyword(s):  
Shear Deformation ◽  
Optimum Design ◽  
Transverse Shear ◽  
Transverse Shear Deformation ◽  
Aircraft Wing

Whirling of Composite-Material Driveshafts Including Bending-Twisting Coupling and Transverse Shear Deformation

1993 ◽  
Author(s):  
Charles W. Bert ◽  
Chun-Do Kim
Keyword(s):  
Composite Material ◽  
Shear Deformation ◽  
Timoshenko Beam ◽  
Transverse Shear ◽  
Critical Speed ◽  
Numerical Results ◽  
Transverse Shear Deformation ◽  
First Order ◽  
Shear Deformable

Abstract A simplified theory for predicting the first-order critical speed of a shear deformable, composite-material driveshaft is presented. The shaft is modeled as a Bresse-Timoshenko beam generalized to include bending-twisting coupling. Numerical results are compared with those for both thin and thick walled shell theories and generalized Bernoulli-Euler theory.

Symmetric Flexural Vibrations of a Clamped Circular Disk

1956 ◽  
Vol 23 (2) ◽  
pp. 319
Author(s):  
H. Deresiewicz
Keyword(s):  
Shear Deformation ◽  
Frequency Spectrum ◽  
Transverse Shear ◽  
Circular Disk ◽  
Transverse Shear Deformation ◽  
Axially Symmetric ◽  
Rotatory Inertia ◽  
Flexural Vibrations ◽  
Clamped Edges

Abstract The frequency spectrum is computed for the case of free, axially symmetric vibrations of a circular disk with clamped edges, using a theory which includes the effects of rotatory inertia and transverse shear deformation.

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