JIS G 1313-2-2012 6875 Method for chemical analysis of ferrochromium -- Part 2 Determination of carbon content《铬铁化学分析方法 第2部分 碳含量测定》.pdf

上传人:boatfragile160 文档编号:1261411 上传时间:2019-09-04 格式:PDF 页数:9 大小:469.57KB
下载 相关 举报
JIS G 1313-2-2012 6875 Method for chemical analysis of ferrochromium -- Part 2 Determination of carbon content《铬铁化学分析方法 第2部分 碳含量测定》.pdf_第1页
第1页 / 共9页
JIS G 1313-2-2012 6875 Method for chemical analysis of ferrochromium -- Part 2 Determination of carbon content《铬铁化学分析方法 第2部分 碳含量测定》.pdf_第2页
第2页 / 共9页
JIS G 1313-2-2012 6875 Method for chemical analysis of ferrochromium -- Part 2 Determination of carbon content《铬铁化学分析方法 第2部分 碳含量测定》.pdf_第3页
第3页 / 共9页
JIS G 1313-2-2012 6875 Method for chemical analysis of ferrochromium -- Part 2 Determination of carbon content《铬铁化学分析方法 第2部分 碳含量测定》.pdf_第4页
第4页 / 共9页
JIS G 1313-2-2012 6875 Method for chemical analysis of ferrochromium -- Part 2 Determination of carbon content《铬铁化学分析方法 第2部分 碳含量测定》.pdf_第5页
第5页 / 共9页
点击查看更多>>
资源描述
展开阅读全文
相关资源
猜你喜欢
  • NASA NACA-ARR-3F23-1943 Wind-tunnel investigation of effect of yaw on lateral-stability characteristics V  symmetrically tapered wing with a circular fuselage having a horizontal a.pdf NASA NACA-ARR-3F23-1943 Wind-tunnel investigation of effect of yaw on lateral-stability characteristics V symmetrically tapered wing with a circular fuselage having a horizontal a.pdf
  • NASA NACA-ARR-3F28-1943 Experimental determination of the yawing moment due to yawing contributed by the wing fuselage and vertical tail of a midwing airplane model《由中置翼飞机模型机翼 机身和垂.pdf NASA NACA-ARR-3F28-1943 Experimental determination of the yawing moment due to yawing contributed by the wing fuselage and vertical tail of a midwing airplane model《由中置翼飞机模型机翼 机身和垂.pdf
  • NASA NACA-ARR-3F29-1943 Wind-tunnel investigation of control-surface characteristics XIV - NACA 0009 airfoil with a 20-percent-chord double plain flap《对操纵面特性14的风洞研究 带有20%翼弦双层普通襟翼的N.pdf NASA NACA-ARR-3F29-1943 Wind-tunnel investigation of control-surface characteristics XIV - NACA 0009 airfoil with a 20-percent-chord double plain flap《对操纵面特性14的风洞研究 带有20%翼弦双层普通襟翼的N.pdf
  • NASA NACA-ARR-3H25-1943 Determination of the damping moment in yawing for tapered wings with partial-span flaps《带有局部翼展襟翼锥形机翼的偏航阻力扭矩测定》.pdf NASA NACA-ARR-3H25-1943 Determination of the damping moment in yawing for tapered wings with partial-span flaps《带有局部翼展襟翼锥形机翼的偏航阻力扭矩测定》.pdf
  • NASA NACA-ARR-3L10-1943 Wind-tunnel investigation of an NACA 23012 airfoil with a 0 30-airfoil-chord double slotted flap《对带有0 30翼弦双开缝襟翼NACA 23012机翼的风洞研究》.pdf NASA NACA-ARR-3L10-1943 Wind-tunnel investigation of an NACA 23012 airfoil with a 0 30-airfoil-chord double slotted flap《对带有0 30翼弦双开缝襟翼NACA 23012机翼的风洞研究》.pdf
  • NASA NACA-ARR-4E31-1944 Torsion tests of stiffened circular cylinders《硬化圆柱体的扭力试验》.pdf NASA NACA-ARR-4E31-1944 Torsion tests of stiffened circular cylinders《硬化圆柱体的扭力试验》.pdf
  • NASA NACA-ARR-E5F07-1945 Heat-transfer tests of aqueous ethylene glycol solutions in an electrically heated tube《含水乙烯乙二醇溶液在电加热管中的热传递试验》.pdf NASA NACA-ARR-E5F07-1945 Heat-transfer tests of aqueous ethylene glycol solutions in an electrically heated tube《含水乙烯乙二醇溶液在电加热管中的热传递试验》.pdf
  • NASA NACA-ARR-L4D03-1944 Wind-tunnel investigation of control-surface characteristics XVI - pressure distribution over an NACA 0009 airfoil with 0 30-airfoil-chord beveled-trailing.pdf NASA NACA-ARR-L4D03-1944 Wind-tunnel investigation of control-surface characteristics XVI - pressure distribution over an NACA 0009 airfoil with 0 30-airfoil-chord beveled-trailing.pdf
  • NASA NACA-ARR-L4I16-1944 A method for predicting the elevator deflection required to land《预测升降机偏向着陆所要求的的方法》.pdf NASA NACA-ARR-L4I16-1944 A method for predicting the elevator deflection required to land《预测升降机偏向着陆所要求的的方法》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > JIS

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1