Wing structure static analysis using superelement
This paper describes the use of superelement for the stress and deflection analysis of a typical fighter wing structure. Three methods of analyses were carried out and compared: practical/theoretical analysis; finite element analysis with the conventional element modeling approach; and finite elemen...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
Elsevier Ltd
2012
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Subjects: | |
Online Access: | View Fulltext in Publisher View in Scopus |
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