航空复合材料结构高速冰雹冲击研究综述
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- 英文论文题名：Review of Study on Impact by High Velocity Hailstone on Aircraft Composite structures
- 论文作者：李俊婷 ; 袁墨飞
- 英文论文作者：Li Junting ; Yuan Mofei ; Management Center of Science and Technology of AVIC Harbin Aircraft Industry Group Co. ; Ltd. ; 32thWorkshop of AVIC Harbin Aircraft Industry Group CO.LTD.
- 年：2016
- 作者机构：中航工业哈尔滨飞机工业集团有限责任公司科技管理中心;中航工业哈尔滨飞机工业集团有限责任公司32车间;
- 论文关键词：航空 ; 复合材料结构 ; 冲击 ; 冰雹
- 英文论文关键词：aircraft ; composite structure ; impact ; hailstone
- 会议召开时间：2016-10-31
- 会议录名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛文集（上册）
- 英文会议录名称：Discovery,Innovation and Communication——Proceedings of 7th CSAA Science and Technology Youth Forum
- 语种：中文
- 分类号：V214.8
- 学会代码：ZGHU
- 会议名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛
- 会议地点：中国广东中山
- 主办单位：中国航空学会
- 学会名称：中国航空学会
- 页数：6
- 文件大小：848k
- 原文格式：O
- 会议级别：全国
摘要
纤维增强聚合物基复合材料在航空结构上的应用范围正在不断扩大,航空复合材料结构易于受到高速冰雹的冲击,这些冲击会在复合材料结构内产生不可见的损伤,从而危害其结构完整性。本文综述了航空复合材料结构的冲击损伤及高速冰雹冲击的研究,并对其未来发展方向做了展望。
The application areas of fiber reinforced polymer composite materials in aircraft structures are enlarging.Aircraft composite structures are susceptible to impact caused by high velocity hailstone.These impacts could produce nonvisible damage in the composite structures,thus damage its structural integrity.Study on impact damage of aircraft composite structures and impact by high velocity hailstone are reviewed in the paper,and its development direction is prospected in the future.
The application areas of fiber reinforced polymer composite materials in aircraft structures are enlarging.Aircraft composite structures are susceptible to impact caused by high velocity hailstone.These impacts could produce nonvisible damage in the composite structures,thus damage its structural integrity.Study on impact damage of aircraft composite structures and impact by high velocity hailstone are reviewed in the paper,and its development direction is prospected in the future.
引文
[1]Schaefer,J T,Levit,J J,Weiss S J,et al.The Frequency of Large Hail over the Contiguous United States[J].Bulletin of the American Meteorological Society,2004:4871-4877.
[2]Flickinger G.Large hail pounds tulsa…again.2 News Tulsa,OK.24 April,2011.http://www.kjrh.com/dpp/news/local_news/larg e-hail-pounds-tulsa...-again
[3]Multiple Storms Pound North Texas with Large Hail.Insurance Journal,26 May,2011.http;//www.insurancejoumal.com/news/southcentral/2011/05/26/200031.htm
[4]Funai S.Hail Ice Impact on Composite Structures at Glancing Angles.University of California,2012.
[5]Rhymer J D.Force Criterion Prediction of Damage for Carbon/Epoxy Composite Panels Impacted by High Velocity Ice.Ph.D.Dissertation,University of California,2012.
[6]Schoeppner G A,Abrate S.Delamination Threshold Loads for Low Velocity Impact on Composite laminates.Composites Part A;Applied Science and Manufacturing.2000(31):903-915.
[7]Davies G,Zhang X.Impact Damage Prediction in Carbon Composite Structures.International Journal of Impact Engineering,1995,16(1):149-170.
[8]Olsson R.Mass Criterion for Wave Controlled Impact Response of Composite Plates.Compos Part a Appl S,2000,31(8):879-887.
[9]Whisler D A.Low Velocity Blunt Impacts on Composite Aircraft Structures.Ms.D.Dissertation,University of California San Diego,2009.
[10]Jackson W C,Poe C C.The Use of Impact Force as a Scale Parameter for the Impact Response of Compostie Laminates.NASA Technical Memorandum 104189,AVSCOM Technical Report 92-B-0011992.
[11]Olsson R.Analytical Model for Delamination Growth during Small Mass Impact on Plates.International Journal of Solids and Structures,2010,47(21):2884-2892.
[12]Kim H,Welch D A,Kedward K T.Experimental Investigation of High Velocity Ice Impacts on Woven Carbon/Epoxy Composite Panels.Composites Part A:Applied Science and Manufacturing,2003,(34):25-41.
[13]Park H,Kim H.Damage Resistance of Single lap Adhesive Composite Joints by Transverse Ice Impact.International Journal of Impact Engineering,2010,37(2):177-84.
[14]Kim H,Keune J N.Compressive Strength of Ice at Impact Strain Rates.J Mater Sci,2007,42(8):2802-2806.
[15]Tippmann J D.Development of a Strain Rate Sensitive Ice Material Model for Hail Ice Impact Simulation.Ms.D.Dissertation,University of California,2011.
[16]Lesser A J,Filippov A G.Mechanisms Governing the Damage Resistance of Laminated Composites Subjected to Low-Velocity Impacts.Materials Research Society symposia proceedings,1996,434;293-298.
[17]Rhymer J,Kim H,Roach D.The Damage Resistance of Quasi-Isotropic Carbon/Epoxy Composite Tape Laminates Impacted by High Velocity Ice.Composites Part A:Applied Science and Manufacturing,2012 DOI:10.1016/j.compositesa.2012,02.017.Available online 3 March 2012.
[18]Daniel I M,Luo J J,Schubel P M,et al.Interfiber/Interlaminar Failure of Composites under Multi-Axial States of Stress.Composite Science and Technology,2009,69:764-771.
[19]Daniel I M,Werner B T,Fenner J S.Strain-RateDependent Failure Criteria for Composites.Composites Science and Technology,2011,71:357-364.
[2]Flickinger G.Large hail pounds tulsa…again.2 News Tulsa,OK.24 April,2011.http://www.kjrh.com/dpp/news/local_news/larg e-hail-pounds-tulsa...-again
[3]Multiple Storms Pound North Texas with Large Hail.Insurance Journal,26 May,2011.http;//www.insurancejoumal.com/news/southcentral/2011/05/26/200031.htm
[4]Funai S.Hail Ice Impact on Composite Structures at Glancing Angles.University of California,2012.
[5]Rhymer J D.Force Criterion Prediction of Damage for Carbon/Epoxy Composite Panels Impacted by High Velocity Ice.Ph.D.Dissertation,University of California,2012.
[6]Schoeppner G A,Abrate S.Delamination Threshold Loads for Low Velocity Impact on Composite laminates.Composites Part A;Applied Science and Manufacturing.2000(31):903-915.
[7]Davies G,Zhang X.Impact Damage Prediction in Carbon Composite Structures.International Journal of Impact Engineering,1995,16(1):149-170.
[8]Olsson R.Mass Criterion for Wave Controlled Impact Response of Composite Plates.Compos Part a Appl S,2000,31(8):879-887.
[9]Whisler D A.Low Velocity Blunt Impacts on Composite Aircraft Structures.Ms.D.Dissertation,University of California San Diego,2009.
[10]Jackson W C,Poe C C.The Use of Impact Force as a Scale Parameter for the Impact Response of Compostie Laminates.NASA Technical Memorandum 104189,AVSCOM Technical Report 92-B-0011992.
[11]Olsson R.Analytical Model for Delamination Growth during Small Mass Impact on Plates.International Journal of Solids and Structures,2010,47(21):2884-2892.
[12]Kim H,Welch D A,Kedward K T.Experimental Investigation of High Velocity Ice Impacts on Woven Carbon/Epoxy Composite Panels.Composites Part A:Applied Science and Manufacturing,2003,(34):25-41.
[13]Park H,Kim H.Damage Resistance of Single lap Adhesive Composite Joints by Transverse Ice Impact.International Journal of Impact Engineering,2010,37(2):177-84.
[14]Kim H,Keune J N.Compressive Strength of Ice at Impact Strain Rates.J Mater Sci,2007,42(8):2802-2806.
[15]Tippmann J D.Development of a Strain Rate Sensitive Ice Material Model for Hail Ice Impact Simulation.Ms.D.Dissertation,University of California,2011.
[16]Lesser A J,Filippov A G.Mechanisms Governing the Damage Resistance of Laminated Composites Subjected to Low-Velocity Impacts.Materials Research Society symposia proceedings,1996,434;293-298.
[17]Rhymer J,Kim H,Roach D.The Damage Resistance of Quasi-Isotropic Carbon/Epoxy Composite Tape Laminates Impacted by High Velocity Ice.Composites Part A:Applied Science and Manufacturing,2012 DOI:10.1016/j.compositesa.2012,02.017.Available online 3 March 2012.
[18]Daniel I M,Luo J J,Schubel P M,et al.Interfiber/Interlaminar Failure of Composites under Multi-Axial States of Stress.Composite Science and Technology,2009,69:764-771.
[19]Daniel I M,Werner B T,Fenner J S.Strain-RateDependent Failure Criteria for Composites.Composites Science and Technology,2011,71:357-364.