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Buckling Load Calculations of the Isotropic Shell A-8 Using a High-Fidelity Hierarchical ApproachAs a step towards developing a new design philosophy, one that moves away from the traditional empirical approach used today in design towards a science-based design technology approach, a test series of 7 isotropic shells carried out by Aristocrat and Babcock at Caltech is used. It is shown how the hierarchical approach to buckling load calculations proposed by Arbocz et al can be used to perform an approach often called 'high fidelity analysis', where the uncertainties involved in a design are simulated by refined and accurate numerical methods. The Delft Interactive Shell DEsign COde (short, DISDECO) is employed for this hierarchical analysis to provide an accurate prediction of the critical buckling load of the given shell structure. This value is used later as a reference to establish the accuracy of the Level-3 buckling load predictions. As a final step in the hierarchical analysis approach, the critical buckling load and the estimated imperfection sensitivity of the shell are verified by conducting an analysis using a sufficiently refined finite element model with one of the current generation two-dimensional shell analysis codes with the advanced capabilities needed to represent both geometric and material nonlinearities.
Document ID
20030002802
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Arbocz, Johann
(Technische Hogeschool Delft, Netherlands)
Starnes, James H.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Structural Mechanics
Report/Patent Number
AIAA Paper 2002-1513
Report Number: AIAA Paper 2002-1513
Meeting Information
Meeting: 43rd AIAA/AMSE/ASCE/AHS Structures, Stuctural Dynamics, and Materials Conference
Location: Denver, CO
Country: United States
Start Date: April 22, 2002
End Date: April 25, 2002
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Civil Engineers, American Helicopter Society, Inc., American Society of Mechanical Engineers
Funding Number(s)
CONTRACT_GRANT: NAG1-2129
Distribution Limits
Public
Copyright
Public Use Permitted.
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