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contributor authorW. G. Flieder
contributor authorJ. C. Loria
contributor authorW. J. Smith
date accessioned2017-05-09T00:30:12Z
date available2017-05-09T00:30:12Z
date copyrightSeptember, 1961
date issued1961
identifier issn0021-8936
identifier otherJAMCAV-25631#409_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/139167
description abstractThe design of propellant loading systems for present-day missiles involves the design of pipelines that can carry cryogenic fluids and requires an additional consideration beyond the conventional analyses for flexibility and dead weight. Because of varying flow conditions and boil-off, these cryogenic lines experience varying fill levels and concomitant temperature gradients which cause these lines to bow; i.e., to assume a uniform curvature of circular arc. If constrained, the thermal-stress distributions which are generated by the temperature gradients will have superposed on them additional stresses, which result from the action of the support constraints. This combination of stresses may be critical and/or the loads on the supports may be excessive. The following analysis investigates these bowing effects, thermal stresses, and indicates the support problems entailed.
publisherThe American Society of Mechanical Engineers (ASME)
titleBowing of Cryogenic Pipelines
typeJournal Paper
journal volume28
journal issue3
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.3641720
journal fristpage409
journal lastpage416
identifier eissn1528-9036
keywordsPipelines
keywordsStress
keywordsThermal stresses
keywordsDesign
keywordsTemperature gradients
keywordsBoiling
keywordsMissiles
keywordsPropellants
keywordsWeight (Mass)
keywordsFlow (Dynamics)
keywordsPlasticity AND Fluids
treeJournal of Applied Mechanics:;1961:;volume( 028 ):;issue: 003
contenttypeFulltext


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