压缩载荷的英文

• compre ive load
• compression load
• compressive loading
• load in compression

• "压缩"英文翻译    compress; condense; reduce; ...
• "载荷"英文翻译    load; loading
• "恒压缩载荷" 英文翻译 :    constant compressive load
• "轴向压缩载荷" 英文翻译 :    axial compression load
• "压缩载荷强度试验" 英文翻译 :    compressive test
• "压缩载荷下使用" 英文翻译 :    compression loading application
• "压缩挠曲载荷" 英文翻译 :    compression deflection load
• "压缩屈服载荷" 英文翻译 :    compressive yield load
• "压缩安全有效载荷" 英文翻译 :    esp(encapsulating security payload
• "有效载荷压缩协议" 英文翻译 :    ipayload compression protocol (ippcp) ip; ipayload compression protocol ip
• "载荷" 英文翻译 :    load; loading◇载荷变化 load fluctuation; variation in load; 载荷装置 load device
• "压缩" 英文翻译 :    compress; condense; reduce; cut down; compression; contraction; compaction; pack; reduction; recompression; hoop (静水压的) 压缩非生产性开支 cut down non-productive expenses; 压缩国内需求 depress [lowering] domestic demand; 压缩机关团体购买力 limiting government institutions' purchase of consumer goods; 压缩不适当进口 reduce inappropriate imports; 压缩一则新闻报道 condense a news story; 压缩比 compression ratio; ratio of compression; 压缩饼干 ship biscuit; pilot bread; hardtack; 压缩成型机 compacting shape machine; 压缩冲程 [机械工程] compression stroke; 压缩处理 compressing; 压缩点火 compressed ignition; [机械工程] compression ignition; 压缩制冷 compression refrigeration; 压缩制冷机 compression refrigerating machine; 压缩作用 compression
• "比载荷" 英文翻译 :    unit load
• "臂载荷" 英文翻译 :    beam load
• "变载荷" 英文翻译 :    alternating load; changing load; fluctuating load; variable load
• "冰载荷" 英文翻译 :    ice load
• "部载荷" 英文翻译 :    compound loading
• "超载荷" 英文翻译 :    over burdening
• "初载荷" 英文翻译 :    initial load
• "单载荷" 英文翻译 :    single point load; single-point load
• "低载荷" 英文翻译 :    deeullage
• "点载荷" 英文翻译 :    point load
• "动载荷" 英文翻译 :    [航空] live load; dynamic load; moving load(ing)
• "端载荷" 英文翻译 :    end load
• "风载荷" 英文翻译 :    wind loading

• Cracks may initiate in compression, and certainly in tension .
  裂缝可能在压缩载荷下形成，当然也可能在拉伸载荷下形成。
• Fracture criterion for ceramic notched elements under compression
  轴向压缩载荷下陶瓷切口件的断裂准则
• It was found that tensile residual stress is a key factor for crack growth under cyclic compression
  结果表明裂尖区域在循环压缩载荷作用下的残余拉伸应力是导致裂纹扩展的重要因素。
• Meanwhile , bauschinger phenomena could be modeled because the grains have random orientation . it was demonstrated that crack could grow under far field cyclic compression load in experiments
  本文对不同几何形状的裂纹在循环压缩载荷下的萌生、扩展行为进行了数值模拟分析。
• Sicp / al matrix composites , with 5 , 15 and 25 % volume fraction of sic particles , were prepared by vacuum hot - pressing sintering processing in this paper . based on mechanics properties , sem observation and energy dispersive x - ray analysis , the interface reaction phenomenon of sicp / al composites made by vacuum hot - pressing sintering , as well as the reinforcement and fracture mechanisms of this composite were analyzed . the dynamic responses of sipc / al composites were studied by a split hopkinson high - speed pressure bar impact system which strain rate was from quasistatic state strain rate ( 3 . 3 10 - 3s - 1 ) to dynamic state strain rate ( 5 . 2 103 s - 1 )
  本研究以武装直升飞机防护装甲材料为研究对象，采用真空热压粉末冶金烧结工艺制备了含sic颗粒体积分数分别为5 、 15和25的sic颗粒增强铝基复合材料，结合其力学性能、扫描电镜和界面微区能谱分析结果，分析了sic _ p al复合材料的真空烧结过程中的界面现象，以及材料增强和断裂机理，并利用hopkinson高速压杆冲击实验系统对其从静态到动态(应变率为3 . 3 10 ~ ( - 3 ) s ~ ( - 1 ) 5 . 2 10 ~ 3s ~ ( - 1 ) )的压缩破坏响应进行了研究，分析了不同体积分数sic _ p al复合材料高应变率压缩载荷下，材料的变形和微观损伤机理，以及利用高速冲击空气炮测定了改复合材料制备剃度复合板的穿透性能。
• This article gives the subsistent ability and the analysis result of intensity after repair in the open field airplane composite material structure by research the intensity , rigid and repair problem under a axis compress loads on a typical three stiffened composite laminate which has a penetrability crack ( a scatter damage ) by a shrapnel
  本文通过飞机典型复合材料三加筋层压板结构在被弹片划开一穿透性切口(离散源损伤)后，在轴向压缩载荷作用下所产生的强度、刚度以及修理问题展开了技术研究及探讨，给出军机复合材料加筋板在弹击后生存力以及外场修理后强度恢复分析结果。
• The main structure stress of the car body is particularly analyzed . it is analyzed and calculated under vertical load case , lengthwise stretch load case , lengthwise compression load case , air pressure power load case , operating load case . result shows : the structure distortion harmonize , strength - weakness positions represent local stress focus
  通过对垂向载荷工况、纵向拉伸载荷工况、纵向压缩载荷工况、气动载荷工况和运用状态垂向载荷工况的分析计算，结果表明：该车钢结构变形协调，强度薄弱部位主要表现为局部应力集中。
• The main research is below : ( 1 ) the influence to intensity and rigid with corner angle ( 60 , 75 and 90 degree ) of crack and the board axes ( 2 ) do a fem stress / strain and crack growth simulation analysis when the corner angle of crack and the board axes is 60 degree ( 3 ) do a intensity resume analysis for the structure which is repaired with a titanium patch in a mechanical way when the corner angle of crack and the board axes is 60 degree through simulation analysis for three failure criterion , we have : ( 1 ) in 60 , damage extend quickly with damage analysis in hashin criterion ; it is slower for analysis in maximum stress or hashin - rotem criterion . ( 2 ) in special term ( physical condition incision , shape or maximum load ) the compression strength of the stiffened plate will decline 45 % ~ 50 % under compression loads
  通过采用三个不同损伤判据的数值仿真模拟，得到如下结论： ( 1 )在60时，用hashin判据进行的损伤分析，损伤扩展较快；最大应力及hashin - rotem判据进行的损伤分析，损伤扩展基本相当，且较慢； ( 2 )在所给加筋板的物理条件、切口大小及形状、最大载荷等一定的条件下，该加筋板在压缩载荷作用下，其压缩强度下降了45 50 ； ( 3 )在本文提及到的机械连接修理方法以及载荷条件下，修理后的结构强度恢复能够满足战时要求。

• 压缩载荷的日语：あっしゅくかじゅう