期刊文献+
共找到10篇文章
< 1 >
每页显示 20 50 100
燃烧条件下影响推进剂脱粘面扩展的因素 被引量:20
1
作者 邢耀国 王立波 +3 位作者 董可海 沈伟 孙臣良 何国强 《推进技术》 EI CAS CSCD 北大核心 2001年第1期77-80,共4页
研究了固体火箭发动机推进剂与包覆层界面脱粘在燃烧条件下扩展的影响因素。对含有预制脱粘面的试件进行了大量的燃烧试验 ,用X射线实时成像系统记录了燃烧过程 ;根据组成试件的不同材料特性 ,分别用粘弹性和线弹性有限元方法计算了试... 研究了固体火箭发动机推进剂与包覆层界面脱粘在燃烧条件下扩展的影响因素。对含有预制脱粘面的试件进行了大量的燃烧试验 ,用X射线实时成像系统记录了燃烧过程 ;根据组成试件的不同材料特性 ,分别用粘弹性和线弹性有限元方法计算了试件在燃烧过程中的应力应变状态 ,并利用修正后的J积分法对脱粘面扩展的可能性进行了预估。理论分析和试验结果均表明 :燃烧室增压速率、脱粘面尺寸、边界条件等因素对脱粘面扩展均有较强的影响。该研究结果对制定固体火箭发动机装药失效判据有一定参考价值。 展开更多
关键词 固体推进剂火箭发动机 推进剂燃烧 衬里 有限元法 脱粘面扩展 包覆层
下载PDF
某端燃固体火箭发动机脱粘面临界尺寸的研究 被引量:1
2
作者 邢耀国 李亚飞 +1 位作者 董可海 刘海峰 《固体火箭技术》 EI CAS CSCD 北大核心 2003年第4期48-51,共4页
建立了含脱粘面的某固体火箭发动机工作过程的数学模型,根据脱粘面不扩展条件下得到的发动机工作过程中压力变化仿真曲线,进行了装药应力应变场的三维粘弹性有限元计算,并采用J积分断裂判据,预估了在发动机工作过程中脱粘面可能发生扩... 建立了含脱粘面的某固体火箭发动机工作过程的数学模型,根据脱粘面不扩展条件下得到的发动机工作过程中压力变化仿真曲线,进行了装药应力应变场的三维粘弹性有限元计算,并采用J积分断裂判据,预估了在发动机工作过程中脱粘面可能发生扩展时的临界尺寸。 展开更多
关键词 燃烧 固体火箭发动机 脱粘面 临界尺寸 导弹 有限元法 装药应力
下载PDF
面芯脱粘缺陷对复合材料夹芯圆柱壳屈曲特性影响分析
3
作者 陈悦 黄静 +1 位作者 朱子旭 李华东 《材料导报》 EI CAS CSCD 北大核心 2024年第5期46-51,共6页
面芯脱粘是复合材料夹芯结构常见的损伤形式。本工作综合考虑面芯界面损伤演化、分层屈曲以及分层扩展的耦合作用,建立了深水静压载荷下复合材料夹芯圆柱壳极限承载能力预报方法。基于非线性极限载荷计算方法,通过预制初始缺陷,开展了... 面芯脱粘是复合材料夹芯结构常见的损伤形式。本工作综合考虑面芯界面损伤演化、分层屈曲以及分层扩展的耦合作用,建立了深水静压载荷下复合材料夹芯圆柱壳极限承载能力预报方法。基于非线性极限载荷计算方法,通过预制初始缺陷,开展了含面芯脱粘缺陷复合材料夹芯圆柱壳屈曲特性分析,揭示了典型面芯脱粘缺陷对复合材料夹芯圆柱壳失效模式及极限承载的影响机理,得到不同面芯脱粘形式、脱粘尺寸、脱粘位置的影响规律。研究发现,随贯穿面芯脱粘长度增加,结构失效模式发生整体屈曲→混合屈曲→局部屈曲演化;外蒙皮/芯层面芯脱粘对含环向贯穿面芯脱粘复合材料夹芯圆柱壳极限承载敏感度更高,内蒙皮/芯层界面脱粘对含纵向贯穿面芯脱粘缺陷复合材料夹芯圆柱壳极限承载敏感度更高;对于多个局部圆形面芯脱粘,沿纵向分布越集中、沿环向分布越离散,结构极限承载损失率越高。研究成果对面芯脱粘缺陷复合材料夹芯圆柱壳的优化设计与可靠性评估具有很好的指导意义。 展开更多
关键词 复合材料 圆柱壳 屈曲 极限承载
下载PDF
漂浮软管接头破损及粘结面脱粘研究 被引量:1
4
作者 魏代锋 安晨 +3 位作者 张哲 徐泽金 高强 李有安 《中国海上油气》 CAS CSCD 北大核心 2023年第4期173-180,共8页
漂浮软管接头在复杂海洋环境作用下,可能发生钢筋破断、层间脱粘和法兰脱落等,危及油气输运安全。为研究漂浮软管接头破损及粘结面失效行为,以某DN 300漂浮软管为例,利用Rebar单元、Embedded嵌入技术和粘聚力接触模型,构建了漂浮软管接... 漂浮软管接头在复杂海洋环境作用下,可能发生钢筋破断、层间脱粘和法兰脱落等,危及油气输运安全。为研究漂浮软管接头破损及粘结面失效行为,以某DN 300漂浮软管为例,利用Rebar单元、Embedded嵌入技术和粘聚力接触模型,构建了漂浮软管接头三维有限元模型,对软管接头在拉伸荷载作用下的力学特性进行研究,并通过有限元分析结果与试验结果的对比验证了数值模拟方法的可行性,进而采用有限元方法分析了漂浮软管接头破损及粘结失效原因。结果表明:①采用Rebar单元和Embedded嵌入技术建立的三维数值模型分析软管接头破损特性是可行的;②软管接头的损伤、脱粘主要是由接头捆扎钢筋破断造成的;③极限轴向拉伸荷载作用下,软管接头的粘结损伤主要发生在距离法兰端面200~672 mm区域,其中570~672 mm区域大部分位置进入完全损伤。研究成果为漂浮软管接头的极限承载设计和泄漏机理研究提供了参考。 展开更多
关键词 漂浮软管 接头破损 捆扎钢筋破断 轴向拉伸荷载
下载PDF
含面芯脱粘缺陷复合材料夹芯梁屈曲失效研究 被引量:3
5
作者 陈悦 朱锡 +1 位作者 李华东 朱子旭 《华中科技大学学报(自然科学版)》 EI CAS CSCD 北大核心 2016年第7期40-45,共6页
为研究面芯脱粘缺陷对复合材料夹层结构屈曲特性的影响,对含贯穿矩形面芯脱粘缺陷的复合材料夹芯梁进行了试验和仿真研究.轴向压缩试验发现:试件破坏模式为混合屈曲失效,承载过程可划分为轴向压缩、局部屈曲、混合屈曲和坍塌失效四个阶... 为研究面芯脱粘缺陷对复合材料夹层结构屈曲特性的影响,对含贯穿矩形面芯脱粘缺陷的复合材料夹芯梁进行了试验和仿真研究.轴向压缩试验发现:试件破坏模式为混合屈曲失效,承载过程可划分为轴向压缩、局部屈曲、混合屈曲和坍塌失效四个阶段.在试验基础上,基于Abaqus非线性弧长算法,对复合材料夹芯梁的极限载荷及后屈曲路径进行模拟.采用三维内聚力单元模拟预制脱粘缺陷,从破坏模式和极限载荷两个方面与试验结果进行对比,误差为6.51%,验证了数值计算方法的可靠性.有限元分析发现:随芯层模量增加,极限荷载先非线性增长后线性增长;当缺陷因子为0.052时,极限荷载为完整结构的80%,为确保结构的承载特性,应在缺陷因子达到0.05前及时进行脱粘区域修补. 展开更多
关键词 复合材料 夹芯梁 缺陷 屈曲 极限荷载
原文传递
EFFECT OF FIBER FAILURE ON QUASI-STATIC UNLOADING/RELOADING HYSTERESIS LOOPS OF CERAMIC MATRIX COMPOSITES 被引量:1
6
作者 李龙彪 宋迎东 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2011年第1期94-102,共9页
The two-parameter Weibull model is used to describe the fiber strength distribution.The stress carried by the intact and fracture fibers on the matrix crack plane during unloading/reloading is determined based on the ... The two-parameter Weibull model is used to describe the fiber strength distribution.The stress carried by the intact and fracture fibers on the matrix crack plane during unloading/reloading is determined based on the global load sharing criterion.The axial stress distribution of intact fibers upon unloading and reloading is determined based on the mechanisms of fiber sliding relative to matrix in the interface debonded region.The interface debonded length,unloading interface counter slip length,and reloading interface new slip length are obtained by the fracture mechanics approach.The hysteresis loops corresponding to different stresses considering fiber failure are compared with the cases without considering fiber failure.The effects of fiber characteristic strength and fiber Weibull modulus on the fiber failure,the shape,and the area of the hysteresis loops are analyzed.The predicted quasi-static unloading/reloading hysteresis loops agree well with experimental data. 展开更多
关键词 ceramic matrix composites hysteresis loops matrix cracking interface debonding fiber failure
下载PDF
Determination of interfacial adhesive properties for polymeric film by blister test 被引量:1
7
作者 王子菡 马增胜 +1 位作者 周益春 卢春生 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2013年第10期3033-3039,共7页
The interfacial adhesive properties ofpolypropylene/stainless steel were studied by the blister test. The polypropylene film with a squared free-standing window was pressured by oil from one side of film. The correspo... The interfacial adhesive properties ofpolypropylene/stainless steel were studied by the blister test. The polypropylene film with a squared free-standing window was pressured by oil from one side of film. The corresponding deformation field was observed by a digital speckle correlation method. The experimental results show that the squared film deforms and debonds from stainless steel with the increase of pressure. The debonding of the squared film in initiates from the center of edge and extends to the comer, and then the deformation of film evolves from square to circle shape. The interfacial adhesive energy of polypropylene/stainless steel is (22.60±1.55) J/m2, which is in agreement with that measured by film with a circular window. 展开更多
关键词 blister test polymeric film interracial adhesive properties DEBONDING whole-filed deformation
下载PDF
Compressive response and microstructural evolution of in-situ TiB_(2)particle-reinforced 7075 aluminum matrix composite 被引量:12
8
作者 Han WANG Hai-ming ZHANG +2 位作者 Zhen-shan CUI Zhe CHEN Dong CHEN 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2021年第5期1235-1248,共14页
The hot forming behavior,failure mechanism,and microstructure evolution of in-situ TiB_(2)particle-reinforced 7075 aluminum matrix composite were investigated by isothermal compression test under different deformation... The hot forming behavior,failure mechanism,and microstructure evolution of in-situ TiB_(2)particle-reinforced 7075 aluminum matrix composite were investigated by isothermal compression test under different deformation conditions of deformation temperatures of 300−450℃ and strain rates of 0.001^(−1)s^(−1).The results demonstrate that the failure behavior of the composite exhibits both particle fracture and interface debonding at low temperature and high strain rate,and dimple rupture of the matrix at high temperature and low strain rate.Full dynamic recrystallization,which improves the composite formability,occurs under conditions of high temperature(450℃)and low strain rate(0.001 s^(−1));the grain size of the matrix after hot compression was significantly smaller than that of traditional 7075Al and ex-situ particle reinforced 7075Al matrix composite.Based on the flow stress curves,a constitutive model describing the relationship of the flow stress,true strain,strain rate and temperature was proposed.Furthermore,the processing maps based on both the dynamic material modeling(DMM)and modified DMM(MDMM)were established to analyze flow instability domain of the composite and optimize hot forming processing parameters.The optimum processing domain was determined at temperatures of 425−450℃ and strain rates of 0.001−0.01 s^(−1),in which the fine grain microstructure can be gained and particle crack and interface debonding can be avoided. 展开更多
关键词 in-situ TiB2 particles aluminum matrix composite hot compression deformation particle fracture interface debonding dynamic recrystallization
下载PDF
Flame Retardancy Evaluation of Nanocomposites Prepared from Sawdust and Montmorillonite Clay
9
作者 Lavern Tendayi Nyamutswa Lilian Tichagwa 《Journal of Earth Science and Engineering》 2014年第9期580-586,共7页
Composites of montmorillonite clay and sawdust were prepared with the desired result being having new materials which burn longer than unmodified sawdust. The three forms of clay used for preparation of composites wer... Composites of montmorillonite clay and sawdust were prepared with the desired result being having new materials which burn longer than unmodified sawdust. The three forms of clay used for preparation of composites were unmodified montmorillonite, mono-ionic montmorillonite and organically modified montmorillonite. Montmorillonite clay was converted to mono-ionic clay by ion exchange with sodium using a sodium chloride solution. The mono-ionic clay was organically modified with an organic surfactant, methyl triphenyl phosphonium bromide. Nanocomposites were then prepared by combining the modified and raw forms of the clay with sawdust. The solution blending method was used to make the nanocomposites. The samples were analysed using thermogravimetric analysis and cone calorimetry. The studies showed that the nanocomposite which was made from sawdust and 1% organically modified clay had the most improved results in terms of burning time and thermal stability, as well as giving a calorific value closest to unmodified sawdust and the least amount of residue. 展开更多
关键词 NANOCOMPOSITES ion exchange solution blending MONTMORILLONITE organic modification.
下载PDF
Stress transfer around a broken fiber in unidirectional fiber-reinforced composites considering matrix damage evolution and interface slipping 被引量:2
10
作者 YANG Zhong ZHANG BoMing +1 位作者 ZHAO Lin SUN XinYang 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2011年第2期296-302,共7页
A shear-lag model is applied to study the stress transfer around a broken fiber within unidirectional fiber-reinforced composites(FRC) subjected to uniaxial tensile loading along the fiber direction.The matrix damage ... A shear-lag model is applied to study the stress transfer around a broken fiber within unidirectional fiber-reinforced composites(FRC) subjected to uniaxial tensile loading along the fiber direction.The matrix damage and interfacial debonding,which are the main failure modes,are considered in the model.The maximum stress criterion with the linear damage evolution theory is used for the matrix.The slipping friction stress is considered in the interfacial debonding region using Coulomb friction theory,in which interfacial clamping stress comes from radial residual stress and mismatch of Poisson's ratios of constituents(fiber and matrix).The stress distributions in the fiber and matrix are obtained by the shear-lag theory added with boundary conditions,which includes force continuity and displacement compatibility constraints in the broken and neighboring intact fibers.The result gives axial stress distribution in fibers and shear stress in the interface and compares the theory reasonably well with the measurement by a polarized light microscope.The relation curves between damage,debonding and ineffective region lengths with external strain loading are obtained. 展开更多
关键词 stress transfer shear-lag damage evolution fiber composite
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部