ONORM S 1811-2001 Testing of textiles - Quantitative analysis of binary mixtures - Triacetae fibres with other fibres - Dichlormethane (methylene chloride) method《纺织品测试 二元混合物的定量分析 .pdf

上传人:unhappyhay135 文档编号:1015768 上传时间:2019-03-20 格式:PDF 页数:6 大小:135.27KB
下载 相关 举报
ONORM S 1811-2001 Testing of textiles - Quantitative analysis of binary mixtures - Triacetae fibres with other fibres - Dichlormethane (methylene chloride) method《纺织品测试 二元混合物的定量分析 .pdf_第1页
第1页 / 共6页
ONORM S 1811-2001 Testing of textiles - Quantitative analysis of binary mixtures - Triacetae fibres with other fibres - Dichlormethane (methylene chloride) method《纺织品测试 二元混合物的定量分析 .pdf_第2页
第2页 / 共6页
ONORM S 1811-2001 Testing of textiles - Quantitative analysis of binary mixtures - Triacetae fibres with other fibres - Dichlormethane (methylene chloride) method《纺织品测试 二元混合物的定量分析 .pdf_第3页
第3页 / 共6页
ONORM S 1811-2001 Testing of textiles - Quantitative analysis of binary mixtures - Triacetae fibres with other fibres - Dichlormethane (methylene chloride) method《纺织品测试 二元混合物的定量分析 .pdf_第4页
第4页 / 共6页
ONORM S 1811-2001 Testing of textiles - Quantitative analysis of binary mixtures - Triacetae fibres with other fibres - Dichlormethane (methylene chloride) method《纺织品测试 二元混合物的定量分析 .pdf_第5页
第5页 / 共6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-TP-2478-1985 Effect of aileron deflections on the aerodynamic characteristics of a semispan model of a subsonic energy-efficient transport《副翼偏转对亚音速节能运输机半翼展模型空气动力特性的影响》.pdf NASA-TP-2478-1985 Effect of aileron deflections on the aerodynamic characteristics of a semispan model of a subsonic energy-efficient transport《副翼偏转对亚音速节能运输机半翼展模型空气动力特性的影响》.pdf
  • NASA-TP-2683-1987 Experimental cavity pressure distributions at supersonic speeds《超音速下实验性空腔压力分布》.pdf NASA-TP-2683-1987 Experimental cavity pressure distributions at supersonic speeds《超音速下实验性空腔压力分布》.pdf
  • NASA-TP-2772-1987 Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing《装配有先进自然层流机翼的全比例通用航空飞机的风洞研究》.pdf NASA-TP-2772-1987 Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing《装配有先进自然层流机翼的全比例通用航空飞机的风洞研究》.pdf
  • NASA-TP-2990-1990 Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model《高升力半翼展飞机模型的实验性和理论性空气动力特性》.pdf NASA-TP-2990-1990 Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model《高升力半翼展飞机模型的实验性和理论性空气动力特性》.pdf
  • NASA-TP-3032-1990 Experimental investigation of porous-floor effects on cavity flow fields at supersonic speeds《在超音速下空腔流场渗透性地板影响的实验性研究》.pdf NASA-TP-3032-1990 Experimental investigation of porous-floor effects on cavity flow fields at supersonic speeds《在超音速下空腔流场渗透性地板影响的实验性研究》.pdf
  • NASA-TP-3110-1991 Measurements of forces moments and pressures on a generic store separating from a box cavity at supersonic speeds《在超音速下和箱腔分离的一般储存力 力矩和压力测量》.pdf NASA-TP-3110-1991 Measurements of forces moments and pressures on a generic store separating from a box cavity at supersonic speeds《在超音速下和箱腔分离的一般储存力 力矩和压力测量》.pdf
  • NASA-TP-3133-1991 Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil《带有自然层流机翼商务喷气机翼的全面半翼展试验》.pdf NASA-TP-3133-1991 Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil《带有自然层流机翼商务喷气机翼的全面半翼展试验》.pdf
  • NASA-TP-3192-1992 Stress concentrations for straight-shank and countersunk holes in plates subjected to tension bending and pin loading《承受拉力 弯曲和销载荷板材的直柄和埋头孔的应力集中》.pdf NASA-TP-3192-1992 Stress concentrations for straight-shank and countersunk holes in plates subjected to tension bending and pin loading《承受拉力 弯曲和销载荷板材的直柄和埋头孔的应力集中》.pdf
  • NASA-TP-3557-1996 Improved Method for Prediction of Attainable Wing Leading-Edge Thrust《机翼前缘可得推力预测的改良方法》.pdf NASA-TP-3557-1996 Improved Method for Prediction of Attainable Wing Leading-Edge Thrust《机翼前缘可得推力预测的改良方法》.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