全部 标题 作者
关键词 摘要

OALib Journal期刊
ISSN: 2333-9721
费用:99美元

查看量下载量

相关文章

更多...
-  2019 

玻璃纤维/酚醛树脂复合材料热响应预报方法玻璃纤维/酚醛树脂复合材料热响应预报方法
Forecasting method for thermal response of glass fiber/phenolic resin composites

DOI: 10.13801/j.cnki.fhclxb.20180819.001

Keywords: 玻璃纤维/酚醛树脂复合材料,热响应,火灾,碳化,有限差分法
glass fiber/phenolic resin composites
,thermal response,fire,carbonization,finite difference method

Full-Text   Cite this paper   Add to My Lib

Abstract:

References

[1]  杨德军, 李旭东. C/C复合材料的热化学烧蚀和温度场耦合分析[J]. 复合材料学报, 2013, 30(2):213-219. YANG D J, LI X D. Coupling analysis of temperature field and thermo-chemical ablation of carbon/carbon composites[J]. Acta Materiae Compositae Sinica, 2013, 30(2):213-219(in Chinese).
[2]  杨德军, 李旭东. 碳化烧蚀材料内部热响应的数值分析[J]. 化工新型材料, 2014(2):139-141. YANG D J, LI X D. Numerical analysis of internal thermal response of carbonized ablation materials[J]. New Chemical Materials, 2014(2):139-141(in Chinese).
[3]  朱燕伟, 孟松鹤, 易法军, 等. 碳/酚醛复合材料烧蚀行为预报方法[J]. 复合材料学报, 2016, 33(5):984-990. ZHU Y W, MENG S H, YI F J, et al. Forecasting method for ablation behaviors of carbon/phenolic composites[J]. Acta Materiae Compositae Sinica, 2016, 33(5):984-990(in Chinese).
[4]  张佐光, 宋焕成. 一种民机装饰用阻燃复合材料的研究[J]. 航空学报, 1996, 17(4):426-430. ZHANG Z G, SONG H C. Study of a fire-resistance composite used in civil aviation[J]. Acta Aeronautica et Astronautica Sinica, 1996, 17(4):426-430(in Chinese).
[5]  马百平, 李翰, 邹田春, 等. 运输类飞机的机身抗烧穿性适航要求解析[J]. 航空工程进展, 2017, 8(3):308-314. MA B P, LI H, ZOU T C, et al. Investigation on fuselage burn-through resistance of transport category airplanes[J]. Advances in Aeronautical Science and Engineering, 2017, 8(3):308-314(in Chinese).
[6]  唐见茂. 航空航天复合材料发展现状及前景[J]. 航天器环境工程, 2013, 30(4):352-359. TANG J M. Current status and trends of advanced composites in aerospace[J]. Spacecraft Environment Engineering, 2013, 30(4):352-359(in Chinese).
[7]  Administration Federal Aviation. Composite aircraft structure:AC:20-107B[S]. Washington D. C.:Federal Aviation Administration, US., 2009.
[8]  KEITH C. Report on the serious incident to Boeing B787-8, ET-AOP London Heathrow Airport 12 July 2013[R]. Hampshire:AAIB, 2015.
[9]  KUNG H C. A mathematical model of wood pyrolysis[J]. Combustion & Flame, 1972, 18(2):185-195.
[10]  HENDERSON J B, WIECEK T E. A mathematical model to predict the thermal response of decomposing, expanding polymer composites[J]. Journal of Composite Materials, 1987, 21(4):373-393.
[11]  GIBSON A G, WU Y S, CHANDLER H W, et al. A model for the thermal performance of thick composite laminates in hydrocarbon fires[J]. Oil & Gas Science & Technology, 2006, 50(1):69-74.
[12]  FEIH S, MATHYS Z, GIBSON A G, et al. Modelling the tension and compression strengths of polymer laminates in fire[J]. Composites Science & Technology, 2007, 67(3-4):551-564.
[13]  FEIH S, MATHYS Z, GIBSON A G, et al. Modelling the compression strength of polymer laminates in fire[J]. Composites Part A:Applied Science & Manufacturing, 2007, 38(11):2354-2365.
[14]  KANDARE E, KANDOLA B K, MCCARTHY E D, et al. Fiber-reinforced epoxy composites exposed to high temperature environments:Part Ⅱ-Modeling mechanical property degradation[J]. Journal of Composite Materials, 2011, 45(14):1511-1521.
[15]  BHAT T, CHEVALI V, LIU X, et al. Fire structural resistance of basalt fibre composite[J]. Composites Part A:Applied Science & Manufacturing, 2015, 71:107-115.
[16]  ANJANG A, CHEVALI V S, KANDARE E, et al. Tension modelling and testing of sandwich composites in fire[J]. Composite Structures, 2014, 113(113):437-445.
[17]  杨德军, 李旭东. 碳/碳复合材料烧蚀热响应的数值分析[J]. 化工新型材料, 2013, 41(10):79-81. YANG D J, LI X D. Numerical analysis of ablative thermal response of carbon/carbon composites[J]. New Chemical Materials, 2013, 41(10):79-81(in Chinese).
[18]  HENDERSON J B, WIEBELT J A, TANT M R. A model for the thermal response of polymer composite materials with experimental verification[J]. Journal of Composite Materials, 1985, 19(6):579-595.
[19]  GIBSON A G. Laminate theory analysis of composites under load in fire[J]. Journal of Composite Materials, 2006, 40(7):639-658.
[20]  BURNS L A, FEIH S, MOURITZ A P. Compression failure of carbon fiber-epoxy laminates in fire[J]. Journal of Aircraft, 2010, 47(2):528-533.
[21]  MCGURN M T, DESJARDIN P E, DODD A B. Thermal modeling of carbon-epoxy laminates in fire environments[J]. International Symposium on Fire Safety Science, 2011:1193-1205.
[22]  SUMMERS P T, LATTIMER B Y, CASE S, et al. Predicting compression failure of composite laminates in fire[J]. Composites Part A:Applied Science & Manufacturing, 2012, 43(5):773-782.
[23]  BHAT T, KANDARE E, GIBSON A G, et al. Compressive softening and failure of basalt fibre composites in fire:Modelling and experimentation[J]. Composite Structures, 2017, 165:15-24.
[24]  TRANCHARD P, SAMYN F, DUQUESNE S, et al. Modelling behavior of a carbon epoxy composite exposed to fire:Part Ⅱ-Comparison with experimental results[J]. Materials, 2017, 10(5):470-483.
[25]  时圣波. 高硅氧/酚醛复合材料的烧蚀机理及热-力学性能研究[D]. 哈尔滨:哈尔滨工业大学, 2013. SHI S B. Ablation mechanism and thermal-mechanical behavior of silica/phenolic composites[D]. Harbin:Harbin Institute of Technology, 2013(in Chinese).
[26]  MOURITZ A P, GIBSON A G. Fire properties of polymer composite materials[M]. Springer:Netherlands, 2006.
[27]  史策. 热传导方程有限差分法的MATLAB实现[J]. 咸阳师范学院学报, 2009, 24(4):27-29. SHI C. Heat conduction equation finite difference method to achieve the MATLAB[J]. Journal of Xianyang Normal University, 2009, 24(4):27-29(in Chinese).
[28]  HENDERSON J B, HAGEN S C. A radiant heat flux apparatus for measuring the thermal response of polymeric materials to high temperatures[J]. Polymer Composites, 1985, 6(6):110-114.

Full-Text

Contact Us

service@oalib.com

QQ:3279437679

WhatsApp +8615387084133