2013
DOI: 10.1002/apj.1746
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Numerical investigation of pressurization performance in cryogenic tank of new‐style launch vehicle

Abstract: The pressurization performance of cryogenic tanks during discharge is investigated by a computational fluid dynamic approach. A series of cases accounting for the effects of various influence factors such as inlet gas temperature, ramp time of inlet gas temperature, wall thickness, outflow rate, injector structure, and liquid supercooling on pressurization behaviors are computed and analyzed successively. Several valuable conclusions have been drawn as follows: (1) Increasing inlet gas temperature, applying a … Show more

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Cited by 11 publications
(1 citation statement)
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“…[29] A remarkable transition from traditional metals to composites was made feasible by the advancement of advanced science, technology, and space materials, allowing for the improvement of space systems using extraordinary lightweight materials. [30][31][32] FRP composites have several uses in cryogenic settings and provide a number of advantages. [33][34][35] FRP composite is used as commercial material for cryogenic tanks and is characterized by thermal cycling and fatigue-thermal loads along with their fracture behavior.…”
Section: Introductionmentioning
confidence: 99%
“…[29] A remarkable transition from traditional metals to composites was made feasible by the advancement of advanced science, technology, and space materials, allowing for the improvement of space systems using extraordinary lightweight materials. [30][31][32] FRP composites have several uses in cryogenic settings and provide a number of advantages. [33][34][35] FRP composite is used as commercial material for cryogenic tanks and is characterized by thermal cycling and fatigue-thermal loads along with their fracture behavior.…”
Section: Introductionmentioning
confidence: 99%