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Analysis and Optimum Design of stiffened shear webs in airframes

Dissertation (MEng (Mechanical and Aeronautical Engineering))--University of Pretoria, 2006.

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Other Authors: Visser, A.G.
Format: Thesis
Published: University of Pretoria 2013
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access_status_str Open Access
author2 Visser, A.G.
author_browse Visser, A.G.
author_facet Visser, A.G.
collection Thesis
dc_rights_str_mv © 2004, University of Pretoria. All rights reserved. The copyright in this work vests in the University of Pretoria. No part of this work may be reproduced or transmitted in any form or by any means, without the prior written permission of the University of Pretoria.
description Dissertation (MEng (Mechanical and Aeronautical Engineering))--University of Pretoria, 2006.
format Thesis
id oai:repository.up.ac.za:2263/23127
institution University of Pretoria (South Africa)
last_indexed 2026-06-10T12:40:28.830Z
license_str Other — see source repository
provenance_str_mv Harvested via OAI-PMH from UPSpace — University of Pretoria Institutional Repository
publishDate 2013
publishDateRange 2013
publishDateSort 2013
publisher University of Pretoria
publisherStr University of Pretoria
record_format dspace
source_str UPSpace — University of Pretoria Institutional Repository
spelling oai:repository.up.ac.za:2263/23127 Analysis and Optimum Design of stiffened shear webs in airframes Visser, A.G. Groenwold, Albert A. upetd@up.ac.za Viljoen, Awie Genetic algorithm Structural optimization Fortran program Shear web Aircraft structures Non-linear finite element analysis Naca Diagonal tension Grisham algorithm Post-buckling analysis UCTD Dissertation (MEng (Mechanical and Aeronautical Engineering))--University of Pretoria, 2006. The analysis and optimum design of stiffened, shear webs in aircraft structures is addressed. The post-buckling behaviour of the webs is assessed using the interactive algorithm developed by Grisham. This method requires only linear finite element analyses, while convergence is typically achieved in as few as five iterations. The Grisham algorithm is extensively compared with empirical analysis methods previously used for aircraft structures and also with a refined, non-linear quasi-static finite element analysis. The Grisham algorithm provides for both compressive buckling in two directions as well as shear buckling, and overcomes some of the conservatism inherent in conventional methods of analysis. In addition, the method is notably less expensive than a complete non-linear finite element analysis, even though global collapse cannot be predicted. While verification of the analysis methodology is the main focus of the stud, an initial investigation into optimization is also made. In optimizing stiffened thin walled structures, the Grisham algorithm is combined with a genetic algorithm. Allowable stress constraints are accommodated using a simple penalty formulation. Mechanical and Aeronautical Engineering unrestricted 2013-09-06T14:38:36Z 2005-01-13 2013-09-06T14:38:36Z 2004-03-03 2006-01-13 2005-01-13 Dissertation Viljoen, A 2004, Analysis and Optimum Design of stiffened shear webs in airframes, MEng dissertation, University of Pretoria, Pretoria, viewed yymmdd < http://hdl.handle.net/2263/23127 > http://hdl.handle.net/2263/23127 http://upetd.up.ac.za/thesis/available/etd-01132005-132131/ © 2004, University of Pretoria. All rights reserved. The copyright in this work vests in the University of Pretoria. No part of this work may be reproduced or transmitted in any form or by any means, without the prior written permission of the University of Pretoria. application/pdf application/pdf application/pdf application/pdf application/pdf application/pdf application/pdf application/pdf application/pdf application/pdf application/pdf University of Pretoria
spellingShingle Genetic algorithm
Structural optimization
Fortran program
Shear web
Aircraft structures
Non-linear finite element analysis
Naca
Diagonal tension
Grisham algorithm
Post-buckling analysis
UCTD
Analysis and Optimum Design of stiffened shear webs in airframes
title Analysis and Optimum Design of stiffened shear webs in airframes
title_full Analysis and Optimum Design of stiffened shear webs in airframes
title_fullStr Analysis and Optimum Design of stiffened shear webs in airframes
title_full_unstemmed Analysis and Optimum Design of stiffened shear webs in airframes
title_short Analysis and Optimum Design of stiffened shear webs in airframes
title_sort analysis and optimum design of stiffened shear webs in airframes
topic Genetic algorithm
Structural optimization
Fortran program
Shear web
Aircraft structures
Non-linear finite element analysis
Naca
Diagonal tension
Grisham algorithm
Post-buckling analysis
UCTD
url http://hdl.handle.net/2263/23127
http://upetd.up.ac.za/thesis/available/etd-01132005-132131/