NF P19-110-1998 Determination of steel stresses in unloaded reinforced components made of autoclaved aerated concrete 《高压蒸养加气混凝土制无负荷钢筋元件钢应力的测定》.pdf

上传人:boatfragile160 文档编号:1003808 上传时间:2019-03-18 格式:PDF 页数:10 大小:370.37KB
下载 相关 举报
NF P19-110-1998 Determination of steel stresses in unloaded reinforced components made of autoclaved aerated concrete 《高压蒸养加气混凝土制无负荷钢筋元件钢应力的测定》.pdf_第1页
第1页 / 共10页
NF P19-110-1998 Determination of steel stresses in unloaded reinforced components made of autoclaved aerated concrete 《高压蒸养加气混凝土制无负荷钢筋元件钢应力的测定》.pdf_第2页
第2页 / 共10页
NF P19-110-1998 Determination of steel stresses in unloaded reinforced components made of autoclaved aerated concrete 《高压蒸养加气混凝土制无负荷钢筋元件钢应力的测定》.pdf_第3页
第3页 / 共10页
NF P19-110-1998 Determination of steel stresses in unloaded reinforced components made of autoclaved aerated concrete 《高压蒸养加气混凝土制无负荷钢筋元件钢应力的测定》.pdf_第4页
第4页 / 共10页
NF P19-110-1998 Determination of steel stresses in unloaded reinforced components made of autoclaved aerated concrete 《高压蒸养加气混凝土制无负荷钢筋元件钢应力的测定》.pdf_第5页
第5页 / 共10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-TN-719-1939 The effects of partial-span slotted flaps on the aerodynamic characteristics of a rectangular and a tapered N A C A 23012 wing《部分展翼的开缝襟翼对矩形和锥形NACA 23012机翼空气动力.pdf NASA NACA-TN-719-1939 The effects of partial-span slotted flaps on the aerodynamic characteristics of a rectangular and a tapered N A C A 23012 wing《部分展翼的开缝襟翼对矩形和锥形NACA 23012机翼空气动力.pdf
  • NASA NACA-TN-730-1939 Wind-tunnel investigation of effect of yaw on lateral-stability characteristics II - rectangular N A C A 23012 wing with a circular fuselage and a fin《偏航对带有圆形.pdf NASA NACA-TN-730-1939 Wind-tunnel investigation of effect of yaw on lateral-stability characteristics II - rectangular N A C A 23012 wing with a circular fuselage and a fin《偏航对带有圆形.pdf
  • NASA NACA-TN-734-1939 Pressure-distribution investigation of an N A C A 0009 airfoil with a 50-percent-chord plain flap and three tabs《带有50%弦普通襟翼和三个标签的NACA 0009机翼的压力分布研究》.pdf NASA NACA-TN-734-1939 Pressure-distribution investigation of an N A C A 0009 airfoil with a 50-percent-chord plain flap and three tabs《带有50%弦普通襟翼和三个标签的NACA 0009机翼的压力分布研究》.pdf
  • NASA NACA-TN-747-1940 Propeller rotation noise due to torque and thrust《由扭矩和推力产生的螺旋桨旋转噪音》.pdf NASA NACA-TN-747-1940 Propeller rotation noise due to torque and thrust《由扭矩和推力产生的螺旋桨旋转噪音》.pdf
  • NASA NACA-TN-752-1940 An investigation of sheet-stiffener panels subjected to compression loads with particular reference to torsionally weak stiffeners《承受压缩荷载特别是扭矩弱加强剂的板硬化剂面板的研究》.pdf NASA NACA-TN-752-1940 An investigation of sheet-stiffener panels subjected to compression loads with particular reference to torsionally weak stiffeners《承受压缩荷载特别是扭矩弱加强剂的板硬化剂面板的研究》.pdf
  • NASA NACA-TN-755-1940 Wind-tunnel investigation of an N A C A 23030 airfoil with various arrangements of slotted flaps《带有开缝襟翼的多种形式NACA 23030机翼的风洞研究》.pdf NASA NACA-TN-755-1940 Wind-tunnel investigation of an N A C A 23030 airfoil with various arrangements of slotted flaps《带有开缝襟翼的多种形式NACA 23030机翼的风洞研究》.pdf
  • NASA NACA-TN-759-1940 Pressure-distribution investigation of an N A C A 0009 airfoil with a 30-percent-chord plain flap and three tabs《带有30%弦的普通襟翼和三个标签的NACA 0009机翼的压力分布研究》.pdf NASA NACA-TN-759-1940 Pressure-distribution investigation of an N A C A 0009 airfoil with a 30-percent-chord plain flap and three tabs《带有30%弦的普通襟翼和三个标签的NACA 0009机翼的压力分布研究》.pdf
  • NASA NACA-TN-763-1940 Wind-tunnel investigation of two airfoils with 25-percent-chord Gwinn and plain flaps《带有25%弦的Gwinn和普通襟翼两个机翼的风洞研究》.pdf NASA NACA-TN-763-1940 Wind-tunnel investigation of two airfoils with 25-percent-chord Gwinn and plain flaps《带有25%弦的Gwinn和普通襟翼两个机翼的风洞研究》.pdf
  • NASA NACA-TN-766-1940 A study of the air movements in two aircraft-engine cylinders《对两个飞机发动机汽缸中空气流动的研究》.pdf NASA NACA-TN-766-1940 A study of the air movements in two aircraft-engine cylinders《对两个飞机发动机汽缸中空气流动的研究》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    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