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Finite element analysis of a wing type structure with experimental verification of results.

Thesis (MScEng) -- Stellenbosch University, 1976.

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Bibliographic Details
Main Author: Baumgartner, Edward Michael Ernst
Other Authors: Fourie, E.
Format: Thesis
Language:en_ZA
Published: Stellenbosch : Stellenbosch University 2012
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access_status_str Open Access
author Baumgartner, Edward Michael Ernst
author2 Fourie, E.
author_browse Baumgartner, Edward Michael Ernst
Fourie, E.
author_facet Fourie, E.
Baumgartner, Edward Michael Ernst
author_sort Baumgartner, Edward Michael Ernst
collection Thesis
dc_rights_str_mv Stellenbosch University
description Thesis (MScEng) -- Stellenbosch University, 1976.
format Thesis
id oai:scholar.sun.ac.za:10019.1/67960
institution Stellenbosch University (South Africa)
language en_ZA
last_indexed 2026-06-10T12:45:46.810Z
license_str Other — see source repository
provenance_str_mv Harvested via OAI-PMH from SUNScholar — Stellenbosch University Repository
publishDate 2012
publishDateRange 2012
publishDateSort 2012
publisher Stellenbosch : Stellenbosch University
publisherStr Stellenbosch : Stellenbosch University
record_format dspace
source_str SUNScholar — Stellenbosch University Repository
spelling oai:scholar.sun.ac.za:10019.1/67960 Finite element analysis of a wing type structure with experimental verification of results. Baumgartner, Edward Michael Ernst Fourie, E. Du Preez, R. J. Stellenbosch University. Faculty of Engineering. Dept. of Electrical & Electronic Engineering. Structural analysis (Engineering) Finite element method Airplanes -- Wings -- Computer programs Dissertations -- Engineering Thesis (MScEng) -- Stellenbosch University, 1976. pt. A. Theory and computer program -- pt. B. Experimental. INTRODUCTION: The advent of the high speed computer has revolutionized structural design in all spheres of Engineering. Up till then structural stress analysis was limited to over-simplification of the structure in question to comply with derived classical mathematical solutions. In practice however the picture is very different, the structure usually being complex and highly redundant in nature. The techniques involving Energy Methods to solve such structures have been known for a long time. However they required weeks of hand calculations to solve only a small number of redundancies in a structure. Neville Shute mentions this in his book Slide Rule. The development of Matrix algebra and the finite element method has made it possible to analyse, say, a complete aircraft structure in a matter of days. using a large capacity high speed computer~ Experimental results have shown that finite element stress analysis comes much closer to reality than the dated classical methods. 2012-08-27T12:26:21Z 2012-08-27T12:26:21Z 1976-06 Thesis http://hdl.handle.net/10019.1/67960 en_ZA Stellenbosch University 2 v. in 1 : ill. application/pdf Stellenbosch : Stellenbosch University
spellingShingle Structural analysis (Engineering)
Finite element method
Airplanes -- Wings -- Computer programs
Dissertations -- Engineering
Baumgartner, Edward Michael Ernst
Finite element analysis of a wing type structure with experimental verification of results.
title Finite element analysis of a wing type structure with experimental verification of results.
title_full Finite element analysis of a wing type structure with experimental verification of results.
title_fullStr Finite element analysis of a wing type structure with experimental verification of results.
title_full_unstemmed Finite element analysis of a wing type structure with experimental verification of results.
title_short Finite element analysis of a wing type structure with experimental verification of results.
title_sort finite element analysis of a wing type structure with experimental verification of results
topic Structural analysis (Engineering)
Finite element method
Airplanes -- Wings -- Computer programs
Dissertations -- Engineering
url http://hdl.handle.net/10019.1/67960
work_keys_str_mv AT baumgartneredwardmichaelernst finiteelementanalysisofawingtypestructurewithexperimentalverificationofresults