Article(id=1323704520206852799, tenantId=1146029695717560320, journalId=1255847867265597444, issueId=1323704504184611387, articleNumber=null, orderNo=null, doi=null, pmid=null, cstr=null, oa=null, hot=null, price=null, onlineType=0, articleFormat=0, articleType=null, articleTypeStr=null, receivedDate=1163692800000, receivedDateStr=2006-11-17, revisedDate=1168358400000, revisedDateStr=2007-01-10, acceptedDate=null, acceptedDateStr=null, onlineDate=1793525350857, onlineDateStr=2026-11-01, pubDate=1196784000000, pubDateStr=2007-12-05, doiRegisterDate=null, doiRegisterDateStr=null, onlineIssueDate=1793525350857, onlineIssueDateStr=2026-11-01, onlineJustAcceptDate=null, onlineJustAcceptDateStr=null, onlineFirstDate=null, onlineFirstDateStr=null, sourceXml=null, magXml=null, createTime=1793525350857, creator=13701087609, updateTime=1793525350857, updator=13701087609, issue=Issue{id=1323704504184611387, tenantId=1146029695717560320, journalId=1255847867265597444, year='2007', volume='21', issue='4', pageStart='337', pageEnd='448', issueExtLink='null', onlineDate='null', pubDate='1196784000000', pubDateStr='2007-12-05', beforeIssueId=null, nextIssueId=null, price=null, status=1, issueComplete=1, articleOrder=1, issueType=-1, specialIssue=null, createTime=1793525347037, creator='13701087609', updateTime=1793525347037, updator='13701087609', preIssue=null, nextIssue=null, articleTotal=null, ext=null, issueFiles=null, downloadFileDto=null}, startPage=347, endPage=353, ext={EN=ArticleExt(id=1323704520403985088, articleId=1323704520206852799, tenantId=1146029695717560320, journalId=1255847867265597444, language=EN, title=Investigation on Damage Characteristics of Thin Al-Plates by Oblique Hypervelocity Impact of Al-Sphere, columnId=null, journalTitle=Chinese Journal of High Pressure Physics, columnName=null, runingTitle=null, highlight=null, articleAbstract=

The oblique hypervelocity impacts of space debris on bumper of spacecrafts were studied through 2017 aluminum spheres impacting on thin 2A12 aluminum alloy sheets at different angles. The penetration hole characteristics of single-wall shields and the ricochet characteristics of projectiles were analyzed. The equations for the hole size of oblique hypervelocity impact penetration into thin aluminum alloy sheets were derived. Impact velocities were 2.58 km/s, 3.56 km/s and 4.31 km/s respectively. Impact angles ranged from 0° to 80°. The results indicated that the penetration hole size in thin aluminum alloy sheets depended on the impact velocity and impact angle. When an aluminum alloy sphere of 3.97 mm diameter impacted at hypervelocity on the thin aluminum alloy sheet of 1 mm thickness at different angles, the critical impact angle was between 30° and 40° in which projectile leaped away from the target partially. As impact angle increased, the maximum ricochet angle decreased, and the distributing area of ricochet debris cloud reduced. Impact velocity has little effect on the penetration hole ellipticity of thin aluminum alloy sheets under oblique hypervelocity impact.

, authors=Gong-Shun GUAN, Yue HA, Bao-Jun PANG, authorsList=Gong-Shun GUAN, Yue HA, Bao-Jun PANG, authorCompany=null, correspAuthors=null, authorNote=null, correspAuthorsNote=null, copyrightStatement=null, copyrightOwner=null, extLink=null, articleAbsUrl=null, sourceXml=null, magXml=null, pdfUrl=null, pdf=null, pdfFileSize=null, pdfExtLink=null, richHtmlUrl=null, mobilePdfUrl=null, reviewReport=null, pdfFirstPage=null, abstractGraph=null, abstractGraphContent=null, abstractVideo=null, citation=null, cebUrl=null, magXmlContent=null, mapNumber=null, fund=null), CN=ArticleExt(id=1323704520630477505, articleId=1323704520206852799, tenantId=1146029695717560320, journalId=1255847867265597444, language=CN, title=铝球弹丸超高速斜撞击薄铝板特性研究, columnId=0, journalTitle=高压物理学报, columnName=, runingTitle=null, highlight=null, articleAbstract=

利用2017铝合金球形弹丸超高速斜撞击2A12铝合金薄板,模拟空间碎片对航天器防护屏的超高速撞击作用。分析了铝合金薄板超高速斜撞击穿孔特性与弹丸滑弹返溅特性,建立了铝合金球形弹丸超高速斜撞击铝合金薄板的穿孔经验公式。弹丸撞击速度分别为2.58、3.56和4.31 km/s,撞击角度为10°~80°。实验结果表明:铝合金薄板超高速斜撞击椭圆穿孔尺寸与撞击速度和撞击角度有关,直径为3.97 mm的铝合金球形弹丸超高速斜撞击厚度为1 mm的铝合金薄板时,发生滑弹返溅的临界撞击角在30°~40°之间。最大滑弹返溅角随着撞击角的增大而逐渐减小,此时滑弹返溅碎片云的影响范围缩小,但破坏能力增强。弹丸撞击速度对铝合金薄板超高速斜撞击穿孔的椭圆度影响较小。

, authors=管公顺, 哈跃, 庞宝君, authorsList=管公顺, 哈跃, 庞宝君, authorCompany=null, correspAuthors=null, authorNote=

管公顺(1969—),男,博士后,主要从事超高速撞击动力学理论、实验及航天器空间碎片防护等研究. E-mail:

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管公顺(1969—),男,博士后,主要从事超高速撞击动力学理论、实验及航天器空间碎片防护等研究. E-mail:

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管公顺(1969—),男,博士后,主要从事超高速撞击动力学理论、实验及航天器空间碎片防护等研究. E-mail:

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铝球弹丸超高速斜撞击薄铝板特性研究
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管公顺 , 哈跃 , 庞宝君
高压物理学报 | 2007,21(4): 347-353
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高压物理学报 | 2007 , 21 (4) : 347 -353
铝球弹丸超高速斜撞击薄铝板特性研究
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管公顺(1969—),男,博士后,主要从事超高速撞击动力学理论、实验及航天器空间碎片防护等研究. E-mail:

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管公顺 , 哈跃, 庞宝君
作者信息
  • 哈尔滨工业大学复合材料与结构研究所,黑龙江 哈尔滨 150080
作者简介:

管公顺(1969—),男,博士后,主要从事超高速撞击动力学理论、实验及航天器空间碎片防护等研究. E-mail:

Investigation on Damage Characteristics of Thin Al-Plates by Oblique Hypervelocity Impact of Al-Sphere
Gong-Shun GUAN , Yue HA, Bao-Jun PANG
Affiliations
  • Research Institute of Composites, Harbin Institute of Technology, Harbin 150080, China
出版时间: 2007-12-05
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利用2017铝合金球形弹丸超高速斜撞击2A12铝合金薄板,模拟空间碎片对航天器防护屏的超高速撞击作用。分析了铝合金薄板超高速斜撞击穿孔特性与弹丸滑弹返溅特性,建立了铝合金球形弹丸超高速斜撞击铝合金薄板的穿孔经验公式。弹丸撞击速度分别为2.58、3.56和4.31 km/s,撞击角度为10°~80°。实验结果表明:铝合金薄板超高速斜撞击椭圆穿孔尺寸与撞击速度和撞击角度有关,直径为3.97 mm的铝合金球形弹丸超高速斜撞击厚度为1 mm的铝合金薄板时,发生滑弹返溅的临界撞击角在30°~40°之间。最大滑弹返溅角随着撞击角的增大而逐渐减小,此时滑弹返溅碎片云的影响范围缩小,但破坏能力增强。弹丸撞击速度对铝合金薄板超高速斜撞击穿孔的椭圆度影响较小。

爆炸力学  /  超高速斜撞击  /  薄铝板  /  穿孔尺寸  /  空间碎片

The oblique hypervelocity impacts of space debris on bumper of spacecrafts were studied through 2017 aluminum spheres impacting on thin 2A12 aluminum alloy sheets at different angles. The penetration hole characteristics of single-wall shields and the ricochet characteristics of projectiles were analyzed. The equations for the hole size of oblique hypervelocity impact penetration into thin aluminum alloy sheets were derived. Impact velocities were 2.58 km/s, 3.56 km/s and 4.31 km/s respectively. Impact angles ranged from 0° to 80°. The results indicated that the penetration hole size in thin aluminum alloy sheets depended on the impact velocity and impact angle. When an aluminum alloy sphere of 3.97 mm diameter impacted at hypervelocity on the thin aluminum alloy sheet of 1 mm thickness at different angles, the critical impact angle was between 30° and 40° in which projectile leaped away from the target partially. As impact angle increased, the maximum ricochet angle decreased, and the distributing area of ricochet debris cloud reduced. Impact velocity has little effect on the penetration hole ellipticity of thin aluminum alloy sheets under oblique hypervelocity impact.

mechanics of explosion  /  hypervelocity oblique impact  /  thin aluminum sheet  /  penetration hole size  /  space debris
管公顺, 哈跃, 庞宝君. 铝球弹丸超高速斜撞击薄铝板特性研究. 高压物理学报, 2007 , 21 (4) : 347 -353 .
Gong-Shun GUAN, Yue HA, Bao-Jun PANG. Investigation on Damage Characteristics of Thin Al-Plates by Oblique Hypervelocity Impact of Al-Sphere[J]. Chinese Journal of High Pressure Physics, 2007 , 21 (4) : 347 -353 .

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2007年第21卷第4期
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  • 接收时间:2006-11-17
  • 首发时间:2026-11-01
  • 出版时间:2007-12-05
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  • 收稿日期:2006-11-17
  • 修回日期:2007-01-10
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    哈尔滨工业大学复合材料与结构研究所,黑龙江 哈尔滨 150080
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2种不同金属材料的力学参数
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属
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种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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