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Free Vibration of Uncertain Unsymmetrically Laminated BeamsMonte Carlo Simulation and Stochastic FEA are used to predict randomness in the free vibration response of thin unsymmetrically laminated beams. For the present study, it is assumed that randomness in the response is only caused by uncertainties in the ply orientations. The ply orientations may become random or uncertain during the manufacturing process. A new 16-dof beam element, based on the first-order shear deformation beam theory, is used to study the stochastic nature of the natural frequencies. Using variational principles, the element stiffness matrix and mass matrix are obtained through analytical integration. Using a random sequence a large data set is generated, containing possible random ply-orientations. This data is assumed to be symmetric. The stochastic-based finite element model for free vibrations predicts the relation between the randomness in fundamental natural frequencies and the randomness in ply-orientation. The sensitivity derivatives are calculated numerically through an exact formulation. The squared fundamental natural frequencies are expressed in terms of deterministic and probabilistic quantities, allowing to determine how sensitive they are to variations in ply angles. The predicted mean-valued fundamental natural frequency squared and the variance of the present model are in good agreement with Monte Carlo Simulation. Results, also, show that variations between plus or minus 5 degrees in ply-angles can affect free vibration response of unsymmetrically and symmetrically laminated beams.
Document ID
20010046859
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Kapania, Rakesh K.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA United States)
Goyal, Vijay K.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Publication Information
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Structural Mechanics
Report/Patent Number
AIAA Paper 2001-1317
Report Number: AIAA Paper 2001-1317
Meeting Information
Meeting: 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit
Location: Seattle, WA
Country: United States
Start Date: April 16, 2001
End Date: April 19, 2001
Sponsors: American Society of Mechanical Engineers, American Society of Civil Engineers, American Helicopter Society, Inc., American Inst. of Aeronautics and Astronautics, Alpha STAR Corp.
Funding Number(s)
CONTRACT_GRANT: NAG1-2277
CONTRACT_GRANT: NAG1-2286
Distribution Limits
Public
Copyright
Public Use Permitted.
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