Fire resistance simulation of loaded deck sandwich panel and deck-bulkhead assembly structures
In this study, fire resistance of a deck sandwich panel and deck-bulkhead assembly structures subject to service mechanical loads and to the action of fire is considered. The deck panel mid-span deflection was chosen as a criterion for the fire resistance assessment of both structures. Two simulatio...
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| Vydáno v: | Composites. Part B, Engineering Ročník 39; číslo 1; s. 191 - 195 |
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| Hlavní autoři: | , , |
| Médium: | Journal Article |
| Jazyk: | angličtina |
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Elsevier Ltd
2008
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| ISSN: | 1359-8368, 1879-1069 |
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| Abstract | In this study, fire resistance of a deck sandwich panel and deck-bulkhead assembly structures subject to service mechanical loads and to the action of fire is considered. The deck panel mid-span deflection was chosen as a criterion for the fire resistance assessment of both structures. Two simulation approaches were employed to determine the deck panel mid-span deflections. In the first approach, the GENOA progressive failure analysis software was used to evaluate the damage in the structure based on the equivalent temperature load profile predicted by thermal analysis. In the second approach, coupled thermal–progressive failure simulation was performed on the structure where the progressive failure analysis was invoked immediately after the temperature redistribution had been calculated for each time interval. In both approaches, the effect of fire on the bottom part of the deck panel was simulated through the application of surface heat fluxes to the bottom of the panel to calculate the equivalent temperature load required for the progressive failure analysis. The calculated mid-span deflection of the simply supported deck sandwich panel, after one-hour exposure to fire, correlated well with the experiment performed at Clemson University. Both the simulation and experimental results show that the mid-span deflection was significantly below the 2-ft deflection limit. In addition, the initiation and propagation of damage and fracture patterns over the deck structures were computed. |
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| AbstractList | In this study, fire resistance of a deck sandwich panel and deck-bulkhead assembly structures subject to service mechanical loads and to the action of fire is considered. The deck panel mid-span deflection was chosen as a criterion for the fire resistance assessment of both structures. Two simulation approaches were employed to determine the deck panel mid-span deflections. In the first approach, the GENOA progressive failure analysis software was used to evaluate the damage in the structure based on the equivalent temperature load profile predicted by thermal analysis. In the second approach, coupled thermal–progressive failure simulation was performed on the structure where the progressive failure analysis was invoked immediately after the temperature redistribution had been calculated for each time interval. In both approaches, the effect of fire on the bottom part of the deck panel was simulated through the application of surface heat fluxes to the bottom of the panel to calculate the equivalent temperature load required for the progressive failure analysis. The calculated mid-span deflection of the simply supported deck sandwich panel, after one-hour exposure to fire, correlated well with the experiment performed at Clemson University. Both the simulation and experimental results show that the mid-span deflection was significantly below the 2-ft deflection limit. In addition, the initiation and propagation of damage and fracture patterns over the deck structures were computed. |
| Author | Mosallam, Ayman Abdi, Frank Qian, Zhongyang |
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| Keywords | D. Thermal analysis C. Computational modelling A. Polymer-matrix-composites (PMCs) B. High-temperature properties Fire |
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| References | Murthy PLN, Chamis CC. Integrated composite analyzer (ICAN): users and programmers manual. NASA Technical Paper 2515; 1986. Chamis (bib6) 1969 Nakazawa S, Dias JB, Spiegel MS. MHOST users’ manual, prepared for NASA Lewis Research Center by MARC Analysis Research Corporation; 1987. (bib2) 1986 Farahmand (bib5) 2000 Structural Design, Analyses, Fabrication, and Testing of the Advanced Enclosed Mast/Sensor System (Advanced Technology Demonstration). Carderock Division of the Naval Surface Warfare Center, Materials Sciences Corporation, Ingalls Shipbuilding, and Seemann Composites. NSWCCD-65-TR-1999/2; August 1999. Gibson, Wright, Wu, Mouritz, Mathys, Gardiner (bib9) 2004; 38 Godines C, Abdi F. Final report of fire resistance simulation of horizontal flat sandwich panel and Deck-Bulkhead T-Joint Assembly with temperature and pressure loads. Office of Naval Research, Contract No: N00014-02-M-0213; 2002. DOD/NASA advanced composites design guide, v1. 1st ed. Prepared under contract F33615-78-C-3203 by Rockwell International Corporation; July 1983. Kennedy, Mock, composite DDG51 FLT IIA helicopter hangar: 24-oz E-glass/vinyl ester material properties, JK-00-01; August 2000. Farahmand (10.1016/j.compositesb.2007.02.022_bib5) 2000 10.1016/j.compositesb.2007.02.022_bib10 10.1016/j.compositesb.2007.02.022_bib7 10.1016/j.compositesb.2007.02.022_bib8 10.1016/j.compositesb.2007.02.022_bib1 Gibson (10.1016/j.compositesb.2007.02.022_bib9) 2004; 38 10.1016/j.compositesb.2007.02.022_bib3 10.1016/j.compositesb.2007.02.022_bib4 Chamis (10.1016/j.compositesb.2007.02.022_bib6) 1969 (10.1016/j.compositesb.2007.02.022_bib2) 1986 |
| References_xml | – reference: DOD/NASA advanced composites design guide, v1. 1st ed. Prepared under contract F33615-78-C-3203 by Rockwell International Corporation; July 1983. – year: 1986 ident: bib2 publication-title: Composite materials for aircraft structures – volume: 38 start-page: 1283 year: 2004 end-page: 1307 ident: bib9 article-title: The integrity of polymer composite during and after fire publication-title: J Compos Mater – reference: Structural Design, Analyses, Fabrication, and Testing of the Advanced Enclosed Mast/Sensor System (Advanced Technology Demonstration). Carderock Division of the Naval Surface Warfare Center, Materials Sciences Corporation, Ingalls Shipbuilding, and Seemann Composites. NSWCCD-65-TR-1999/2; August 1999. – year: 2000 ident: bib5 article-title: Durability and damage tolerance of composites publication-title: Welded joints, and bolted joints composites – reference: Murthy PLN, Chamis CC. Integrated composite analyzer (ICAN): users and programmers manual. NASA Technical Paper 2515; 1986. – year: 1969 ident: bib6 article-title: Failure criteria for filamentary composites, composite materials testing and design: ASTM STP 460 – reference: Kennedy, Mock, composite DDG51 FLT IIA helicopter hangar: 24-oz E-glass/vinyl ester material properties, JK-00-01; August 2000. – reference: Nakazawa S, Dias JB, Spiegel MS. MHOST users’ manual, prepared for NASA Lewis Research Center by MARC Analysis Research Corporation; 1987. – reference: Godines C, Abdi F. Final report of fire resistance simulation of horizontal flat sandwich panel and Deck-Bulkhead T-Joint Assembly with temperature and pressure loads. Office of Naval Research, Contract No: N00014-02-M-0213; 2002. – ident: 10.1016/j.compositesb.2007.02.022_bib3 – ident: 10.1016/j.compositesb.2007.02.022_bib4 – year: 1969 ident: 10.1016/j.compositesb.2007.02.022_bib6 – ident: 10.1016/j.compositesb.2007.02.022_bib1 – ident: 10.1016/j.compositesb.2007.02.022_bib10 – ident: 10.1016/j.compositesb.2007.02.022_bib7 – ident: 10.1016/j.compositesb.2007.02.022_bib8 – year: 1986 ident: 10.1016/j.compositesb.2007.02.022_bib2 – year: 2000 ident: 10.1016/j.compositesb.2007.02.022_bib5 article-title: Durability and damage tolerance of composites – volume: 38 start-page: 1283 issue: 15 year: 2004 ident: 10.1016/j.compositesb.2007.02.022_bib9 article-title: The integrity of polymer composite during and after fire publication-title: J Compos Mater doi: 10.1177/0021998304042733 |
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| SubjectTerms | A. Polymer-matrix-composites (PMCs) B. High-temperature properties C. Computational modelling D. Thermal analysis Fire |
| Title | Fire resistance simulation of loaded deck sandwich panel and deck-bulkhead assembly structures |
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