GB T 11805-2019 水轮发电机组自动化元件(装置)及其系统基本技术条件.pdf

上传人:吴艺期 文档编号:1407985 上传时间:2019-12-09 格式:PDF 页数:28 大小:1.31MB
下载 相关 举报
GB T 11805-2019 水轮发电机组自动化元件(装置)及其系统基本技术条件.pdf_第1页
第1页 / 共28页
GB T 11805-2019 水轮发电机组自动化元件(装置)及其系统基本技术条件.pdf_第2页
第2页 / 共28页
GB T 11805-2019 水轮发电机组自动化元件(装置)及其系统基本技术条件.pdf_第3页
第3页 / 共28页
GB T 11805-2019 水轮发电机组自动化元件(装置)及其系统基本技术条件.pdf_第4页
第4页 / 共28页
GB T 11805-2019 水轮发电机组自动化元件(装置)及其系统基本技术条件.pdf_第5页
第5页 / 共28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-L5A05-1945 An empirical formula for the critical shear stress of curved sheets《弯曲板的临界剪切应力经验公式》.pdf NASA NACA-ARR-L5A05-1945 An empirical formula for the critical shear stress of curved sheets《弯曲板的临界剪切应力经验公式》.pdf
  • NASA NACA-ARR-L5B10-1945 Effect of normal pressure on the critical compressive and shear stress of curved sheet.pdf NASA NACA-ARR-L5B10-1945 Effect of normal pressure on the critical compressive and shear stress of curved sheet.pdf
  • NASA NACA-ARR-L5C01-1945 Wind-tunnel investigation of control-surface characteristics XXI  medium and large aerodynamic balances of two nose shapes and a plain overhang used with aoil.pdf NASA NACA-ARR-L5C01-1945 Wind-tunnel investigation of control-surface characteristics XXI medium and large aerodynamic balances of two nose shapes and a plain overhang used with aoil.pdf
  • NASA NACA-ARR-L5C24-1945 Low-pressure boundary-layer control in diffusers and bends《扩散器和弯曲的低压边界层控制》.pdf NASA NACA-ARR-L5C24-1945 Low-pressure boundary-layer control in diffusers and bends《扩散器和弯曲的低压边界层控制》.pdf
  • NASA NACA-ARR-L5F06-1945 Wind-tunnel investigation of control-surface characteristics XXII - medium and large aerodynamic balances of two nose shapes and a plain overhang used withrfoi.pdf NASA NACA-ARR-L5F06-1945 Wind-tunnel investigation of control-surface characteristics XXII - medium and large aerodynamic balances of two nose shapes and a plain overhang used withrfoi.pdf
  • NASA NACA-ARR-L5G25-1945 Wind tunnel investigation of control-surface characteristics XXIII  a 0 25-airfoil-chord flap with tab having a chord twice the flap chord on an NACA 0009 .pdf NASA NACA-ARR-L5G25-1945 Wind tunnel investigation of control-surface characteristics XXIII a 0 25-airfoil-chord flap with tab having a chord twice the flap chord on an NACA 0009 .pdf
  • NASA NACA-ARR-L6A05-1946 Charts for critical combinations of longitudinal and transverse direct stress for flat rectangular plates《平面矩形板纵向和横向直接应力临界组合图》.pdf NASA NACA-ARR-L6A05-1946 Charts for critical combinations of longitudinal and transverse direct stress for flat rectangular plates《平面矩形板纵向和横向直接应力临界组合图》.pdf
  • NASA NACA-CB-5B05-1945 Computation of hinge-moment characteristics of horizontal tails from section data《根据截面数据对水平尾翼铰链力矩特性的计算》.pdf NASA NACA-CB-5B05-1945 Computation of hinge-moment characteristics of horizontal tails from section data《根据截面数据对水平尾翼铰链力矩特性的计算》.pdf
  • NASA NACA-CB-L4G10-1944 Wind tunnel investigation of NACA 66(215)-216 66 1-212 and 65(sub 1)-212 airfoils with 0 20-airfoil-chord split flaps《对带有0 20翼弦分裂式襟翼NACA 66(215)-216 66 1-21.pdf NASA NACA-CB-L4G10-1944 Wind tunnel investigation of NACA 66(215)-216 66 1-212 and 65(sub 1)-212 airfoils with 0 20-airfoil-chord split flaps《对带有0 20翼弦分裂式襟翼NACA 66(215)-216 66 1-21.pdf
  • 相关搜索
    资源标签

    当前位置:首页 > 标准规范 > 国家标准

    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