Problems encountered when idealizing complex aircraft structures into discrete elements for purpose of matrix stress analysis are reviewed, such as problems arising in analysis of wing-type structures by matrix displacement method; problems encountered in analyzing fuselage structures by matrix force method; some results of controlled studies of idealization variations are presented.
Some problems in discrete element representation of aircraft structures
AGARDograph
AGARDograph ; p 267-315
1964
49 pages
Report
Englisch
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