NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Design Optimization of Stiffened Panels with Postbuckling ConstraintsThe funding provided by the grant is used to complete the final stages of the development of a geometrically nonlinear analysis and design capability for the static response of compressively loaded prismatic plate structures. The analysis is based on the nonlinear finite strip method and is applicable for structures, such as stiffened panels or box columns, that can be modeled as assemblages of finite length plate strips. In an effort to reduce the computational cost of the nonlinear finite strip method, thus making it suitable for use in the design optimization environment, reduced basis techniques as described in various references by Noor are used in conjunction with the finite strip method. In addition, an efficient scheme for tracing the nonlinear equilibrium paths through highly nonlinear response curves was implemented. The new scheme, which is referred to as the normal flow algorithm, is based on homotopy methods, and is capable of negotiating highly nonlinear limit point instabilities with a reduced computational cost compared to the popular Ricks/Wempner and Chrisfield algorithms.
Document ID
20000023202
Acquisition Source
Langley Research Center
Document Type
Contractor or Grantee Report
Authors
Guerdal, Zafer
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA United States)
Ragon, Scott
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1999
Subject Category
Structural Mechanics
Funding Number(s)
CONTRACT_GRANT: NAG1-2116
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available