SIS SS 83 41 36-1979 Furnishing and fittings for housing Storage units Floor units《住房家具和配件 存储单元 地板单元》.pdf

上传人:花仙子 文档编号:1042013 上传时间:2019-03-24 格式:PDF 页数:2 大小:44.25KB
下载 相关 举报
SIS SS 83 41 36-1979 Furnishing and fittings for housing  Storage units  Floor units《住房家具和配件 存储单元 地板单元》.pdf_第1页
第1页 / 共2页
SIS SS 83 41 36-1979 Furnishing and fittings for housing  Storage units  Floor units《住房家具和配件 存储单元 地板单元》.pdf_第2页
第2页 / 共2页
亲,该文档总共2页,全部预览完了,如果喜欢就下载吧!
资源描述
展开阅读全文
相关资源
猜你喜欢
  • NASA-TN-D-523-1960 Investigation of the flow in a rectangular cavity in a flat plate at a mach number of 3 55《当马赫数为3 55时 平板中举行空腔中气流的研究》.pdf NASA-TN-D-523-1960 Investigation of the flow in a rectangular cavity in a flat plate at a mach number of 3 55《当马赫数为3 55时 平板中举行空腔中气流的研究》.pdf
  • NASA-TN-D-5361-1969 Analysis of lateral-directional stability characteristics of a twin-jet fighter airplane at high angles of attack《在高攻角时 双喷气战斗机的横向航向稳定特性的分析》.pdf NASA-TN-D-5361-1969 Analysis of lateral-directional stability characteristics of a twin-jet fighter airplane at high angles of attack《在高攻角时 双喷气战斗机的横向航向稳定特性的分析》.pdf
  • NASA-TN-D-5364-1969 Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap《装配有外流喷气襟翼的短距离起落飞机结构的风洞研究》.pdf NASA-TN-D-5364-1969 Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap《装配有外流喷气襟翼的短距离起落飞机结构的风洞研究》.pdf
  • NASA-TN-D-5390-1969 Effect of stress ratio on fatigue-crack growth in 7075-T6 and 2024-T3 aluminum-alloy specimens《应力比对7075-T6和2024-T3铝合金样品疲劳裂缝扩展的影响》.pdf NASA-TN-D-5390-1969 Effect of stress ratio on fatigue-crack growth in 7075-T6 and 2024-T3 aluminum-alloy specimens《应力比对7075-T6和2024-T3铝合金样品疲劳裂缝扩展的影响》.pdf
  • NASA-TN-D-5392-1969 Experimental pressure distributions for a family of blunt bodies at Mach numbers from 2 49 to 4 63 and angles of attack from 0 degrees to 15 degrees《当马赫数为2 49至4.pdf NASA-TN-D-5392-1969 Experimental pressure distributions for a family of blunt bodies at Mach numbers from 2 49 to 4 63 and angles of attack from 0 degrees to 15 degrees《当马赫数为2 49至4.pdf
  • NASA-TN-D-5408-1969 Static and dynamic stability derivatives of a model of a jet transport equipped with external-flow jet-augmented flaps《装配有外流喷气扩张襟翼喷气运输机模型的静态和动态稳定性导数》.pdf NASA-TN-D-5408-1969 Static and dynamic stability derivatives of a model of a jet transport equipped with external-flow jet-augmented flaps《装配有外流喷气扩张襟翼喷气运输机模型的静态和动态稳定性导数》.pdf
  • NASA-TN-D-5467-1969 Discharge coefficients for thick plate orifices with approach flow perpendicular and inclined to the orifice axis《带有和孔口轴垂直和倾向于孔口轴的迎风气流厚板孔口的流量系数》.pdf NASA-TN-D-5467-1969 Discharge coefficients for thick plate orifices with approach flow perpendicular and inclined to the orifice axis《带有和孔口轴垂直和倾向于孔口轴的迎风气流厚板孔口的流量系数》.pdf
  • NASA-TN-D-548-1960 Atmospheric Turbulence Measurements Obtained from Airplane Operations at Altitudes Between 20 000 and 75 000 Feet for Several Areas in the Northern Hemisphere《从北.pdf NASA-TN-D-548-1960 Atmospheric Turbulence Measurements Obtained from Airplane Operations at Altitudes Between 20 000 and 75 000 Feet for Several Areas in the Northern Hemisphere《从北.pdf
  • NASA-TN-D-55-1960 Wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range including effect.pdf NASA-TN-D-55-1960 Wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range including effect.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