1963
DOI: 10.21236/ad0423524
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Tests of Ring-Stiffened and Sandwich Composite Cylinders Under External Hydrostatic Pressure

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1967
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Cited by 13 publications
(13 citation statements)
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“…Many of the models ruptured during collapse. Models labelled SS-43 through SS-56 [12] did not collapse and did not rupture, though buckling was observed. The test on each model did not end until the centre deflection was greater than the initial rise of the dome.…”
Section: Krenzke and Kiernan [12] And [13]mentioning
confidence: 94%
See 1 more Smart Citation
“…Many of the models ruptured during collapse. Models labelled SS-43 through SS-56 [12] did not collapse and did not rupture, though buckling was observed. The test on each model did not end until the centre deflection was greater than the initial rise of the dome.…”
Section: Krenzke and Kiernan [12] And [13]mentioning
confidence: 94%
“…The largest set of tests appears to have been those of Krenzke & Kiernan [12,13], published in 1963. A total of 73 clamped spherical aluminium dome models were tested with included angles ranging from 5 to 120 degrees.…”
Section: Krenzke and Kiernan [12] And [13]mentioning
confidence: 99%
“…Krenzke and Kiernan (1963) proposed γ = 0.7 as an empirical lower-bound knockdown factor for designing spherical shells. However, it was later argued that early experimental results were too scattered, mainly due to the lack of precise control of imperfections during fabrication (Kaplan and Fung, 1954;Homewood et.…”
Section: Accepted Manuscriptmentioning
confidence: 99%
“…However, it has been found that the buckling pressure of stiffened spherical shells is actually smaller than for unstiffened shells with the same weight (Krenzke and Kiernan, 1963). Other configurations of the stiffeners may perform better, but the number of studies of externally pressurized, stiffened spherical shells is currently quite limited (Singer et al, 2002;Ventsel and Krauthammer, 2001).…”
Section: A C C E P T E D Mmentioning
confidence: 99%
“…However, sufficient experimental work has been conducted to indicate that potential weight savings can be achieved if stiffeners are spaced at relatively close intervals and distributed in a particular array or grid-like pattern. 2 , 3 On the other hand, when the unsupported arc length between * stiffeners is large, stiffening systems may be ineffective and may even weaken the shell.…”
Section: Introductionmentioning
confidence: 99%