2002
DOI: 10.1016/s0950-4230(02)00019-0
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Computational modeling of vapor cloud explosions in off-shore rigs using a flame-speed based combustion model

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Cited by 10 publications
(5 citation statements)
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“…In previous work with CEBAM where only gas phase material was present, a Steger-Warming flux vector splitting scheme, as described in [10,11] was used. Simulations using this scheme in CEBAM have been documented in [1][2][3]. This also has proven accurate for the HE scenarios in air presented here.…”
Section: Numerical Formulationmentioning
confidence: 78%
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“…In previous work with CEBAM where only gas phase material was present, a Steger-Warming flux vector splitting scheme, as described in [10,11] was used. Simulations using this scheme in CEBAM have been documented in [1][2][3]. This also has proven accurate for the HE scenarios in air presented here.…”
Section: Numerical Formulationmentioning
confidence: 78%
“…It is titled the Computational Explosion and Blast Assessment Model (CEBAM) and is based on an earlier version developed for vapor cloud explosions (VCEs). The fundamentals of the code as used for VCEs are described in [1], while [2,3] show comparisons of CEBAM predictions with large scale explosion data. Clutter et al [4] reviews use of the code in facility scale accident investigations which include many of the same tasks as found in vulnerability assessments.…”
Section: Computational Modelmentioning
confidence: 99%
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“…Here its capabilities in addressing high-explosive events are briefly reviewed. It can also be used for vapor cloud explosion (VCE) scenarios [3].…”
Section: C Cu Ur Rr Re En Nt T C Co Om Mp Pu Ut Ta At Ti Io On Nmentioning
confidence: 99%
“…Up to now, influencing factors of the overpressure of fuel-air cloud have been widely studied. Some works on the enclosed space have paid attention to the influencing factors of the overpressure production process of gas-liquid twophase, gas-solid two-phase, and gas-liquid-solid three-phase within the vessel in laboratory [2][3][4][5][6][7], such as the location of the detonation initiation point [8,9], energy [10] and ignition way [11], particle size [12] of fuel-air mixtures, and fuel type [13]. Moreover, the related computational model had been established [8,14].…”
Section: Introductionmentioning
confidence: 99%