WJ Z 431-2005 Safety requirement criteria for individual soldier information system《单兵综合作战信息系统安全设计要求》.pdf

上传人:unhappyhay135 文档编号:1288665 上传时间:2019-09-16 格式:PDF 页数:12 大小:451.53KB
下载 相关 举报
WJ Z 431-2005 Safety requirement criteria for individual soldier information system《单兵综合作战信息系统安全设计要求》.pdf_第1页
第1页 / 共12页
WJ Z 431-2005 Safety requirement criteria for individual soldier information system《单兵综合作战信息系统安全设计要求》.pdf_第2页
第2页 / 共12页
WJ Z 431-2005 Safety requirement criteria for individual soldier information system《单兵综合作战信息系统安全设计要求》.pdf_第3页
第3页 / 共12页
WJ Z 431-2005 Safety requirement criteria for individual soldier information system《单兵综合作战信息系统安全设计要求》.pdf_第4页
第4页 / 共12页
WJ Z 431-2005 Safety requirement criteria for individual soldier information system《单兵综合作战信息系统安全设计要求》.pdf_第5页
第5页 / 共12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-RM-L8K19-1949 Wind-tunnel investigation at low speeds of various plug-aileron and lift-flap configurations on a 42 degrees sweptback semispan wing《低速下 42半翼展后掠翼上多种插头副翼和升力襟.pdf NASA NACA-RM-L8K19-1949 Wind-tunnel investigation at low speeds of various plug-aileron and lift-flap configurations on a 42 degrees sweptback semispan wing《低速下 42半翼展后掠翼上多种插头副翼和升力襟.pdf
  • NASA NACA-RM-L8K22-1949 Two-dimensional wind-tunnel investigation of two NACA 6-series airfoils with leading-edge slats《带有前缘缝翼的NACA第6系列机翼的二维风洞研究》.pdf NASA NACA-RM-L8K22-1949 Two-dimensional wind-tunnel investigation of two NACA 6-series airfoils with leading-edge slats《带有前缘缝翼的NACA第6系列机翼的二维风洞研究》.pdf
  • NASA NACA-RM-L8L29-1949 Low-speed static-stability and rolling characteristics of low-aspect-ratio wings of triangular and modified triangular plan forms《三角形和改良三角形平面低展弦比机翼的低速静态稳定性和.pdf NASA NACA-RM-L8L29-1949 Low-speed static-stability and rolling characteristics of low-aspect-ratio wings of triangular and modified triangular plan forms《三角形和改良三角形平面低展弦比机翼的低速静态稳定性和.pdf
  • NASA NACA-RM-L9A07-1949 Low-speed investigation of aileron and spoiler characteristics of a wing having 42 degrees sweepback of the leading edge and circular-arc airfoil sections aexp .pdf NASA NACA-RM-L9A07-1949 Low-speed investigation of aileron and spoiler characteristics of a wing having 42 degrees sweepback of the leading edge and circular-arc airfoil sections aexp .pdf
  • NASA NACA-RM-L9B02-1949 Full-scale investigation of a wing with the leading edge swept back 47 5 degrees and having circular-arc and finite-trailing-edge-thickness ailerons《带有前缘47 .pdf NASA NACA-RM-L9B02-1949 Full-scale investigation of a wing with the leading edge swept back 47 5 degrees and having circular-arc and finite-trailing-edge-thickness ailerons《带有前缘47 .pdf
  • NASA NACA-RM-L9D06-1949 Wing-tunnel investigation at high subsonic speeds of the lateral-control characteristics of an aileron and a stepped spoiler on a wing with leading edge swe.pdf NASA NACA-RM-L9D06-1949 Wing-tunnel investigation at high subsonic speeds of the lateral-control characteristics of an aileron and a stepped spoiler on a wing with leading edge swe.pdf
  • NASA NACA-RM-L9E02-1949 The effect of span and deflection of split flaps and leading-edge roughness on the longitudinal stability and gliding characteristics of a 42 degrees sweptb襟.pdf NASA NACA-RM-L9E02-1949 The effect of span and deflection of split flaps and leading-edge roughness on the longitudinal stability and gliding characteristics of a 42 degrees sweptb襟.pdf
  • NASA NACA-RM-L9E10-1949 Effects of Mach number and sweep on the damping-in-roll characteristics of wings of aspect ratio 4《马赫数和扫掠对展弦比为4的机翼滚转阻尼特性的影响》.pdf NASA NACA-RM-L9E10-1949 Effects of Mach number and sweep on the damping-in-roll characteristics of wings of aspect ratio 4《马赫数和扫掠对展弦比为4的机翼滚转阻尼特性的影响》.pdf
  • NASA NACA-RM-L9E24-1949 Investigation of low-speed aileron control characteristics at a Reynolds number of 6 800 000 of a wing with leading edge swept back 42 degrees with and with.pdf NASA NACA-RM-L9E24-1949 Investigation of low-speed aileron control characteristics at a Reynolds number of 6 800 000 of a wing with leading edge swept back 42 degrees with and with.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 行业标准 > WJ兵器行业

    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