2006
DOI: 10.2514/1.5429
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Shell Buckling Design Criteria Based on Manufacturing Imperfection Signatures

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Cited by 100 publications
(27 citation statements)
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“…Cf. also similar computational results by Hilburger et al (Figures 7 and 8 in [57]) for the transient postbuckling behaviour of a quasi-isotropic cylinder with measured imperfections.…”
Section: Numerical Simulations Of Buckling Behavioursupporting
confidence: 86%
“…Cf. also similar computational results by Hilburger et al (Figures 7 and 8 in [57]) for the transient postbuckling behaviour of a quasi-isotropic cylinder with measured imperfections.…”
Section: Numerical Simulations Of Buckling Behavioursupporting
confidence: 86%
“…Due to the absence of fast and reliable methodologies to calculate the knock-down factor of cylindrical shells under compressive loads, some authors like Hilburger et al [3] and Degenhardt et al [4] and [5] opted for fully detailed numerical models including different types of geometrical imperfections: mid-surface imperfection and thickness imperfection.…”
Section: Desicos Project (New Robust Design Guideline For Imperfectiomentioning
confidence: 99%
“…Nonetheless, despite significant theoretical and computational efforts in understanding imperfection sensitivity, practical designs of curved shells have traditionally made use of empirical knockdown factors [11,12]. In contrast to this approach, efforts currently underway by NASA and others in the aerospace industry aim at developing deterministic design guidelines based on manufacturing-specific imperfection distribution [13][14][15].…”
Section: Introductionmentioning
confidence: 99%