NEN 3235 9 2 1-1978 Test methods tor waste water Gravimetric determination of oil and fat content Soxhlet extraction《废水试验方法 含油脂率的重量法测定 索格利特(Soxhlet extraction)萃取》.pdf

上传人:amazingpat195 文档编号:995326 上传时间:2019-03-16 格式:PDF 页数:4 大小:86.93KB
下载 相关 举报
NEN 3235 9 2 1-1978 Test methods tor waste water Gravimetric determination of oil and fat content Soxhlet extraction《废水试验方法 含油脂率的重量法测定 索格利特(Soxhlet extraction)萃取》.pdf_第1页
第1页 / 共4页
NEN 3235 9 2 1-1978 Test methods tor waste water Gravimetric determination of oil and fat content Soxhlet extraction《废水试验方法 含油脂率的重量法测定 索格利特(Soxhlet extraction)萃取》.pdf_第2页
第2页 / 共4页
NEN 3235 9 2 1-1978 Test methods tor waste water Gravimetric determination of oil and fat content Soxhlet extraction《废水试验方法 含油脂率的重量法测定 索格利特(Soxhlet extraction)萃取》.pdf_第3页
第3页 / 共4页
NEN 3235 9 2 1-1978 Test methods tor waste water Gravimetric determination of oil and fat content Soxhlet extraction《废水试验方法 含油脂率的重量法测定 索格利特(Soxhlet extraction)萃取》.pdf_第4页
第4页 / 共4页
亲,该文档总共4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 NACA-TN-1187-1947 Formulas for additional mass corrections to the moments of inertia of airplanes《附加质量更正和飞机惯性力矩的公式》.pdf NASA NACA-TN-1187-1947 Formulas for additional mass corrections to the moments of inertia of airplanes《附加质量更正和飞机惯性力矩的公式》.pdf
  • NASA NACA-TN-1191-1947 Two-dimensional wind-tunnel investigation of four types of high-lift flap on an NACA 65-210 airfoil section《NACA 65-210翼剖面上四种类型高升力襟翼的二维风洞研究》.pdf NASA NACA-TN-1191-1947 Two-dimensional wind-tunnel investigation of four types of high-lift flap on an NACA 65-210 airfoil section《NACA 65-210翼剖面上四种类型高升力襟翼的二维风洞研究》.pdf
  • NASA NACA-TN-1193-1947 Effect of product of inertia on lateral stability《惯性积对横向稳定性的影响》.pdf NASA NACA-TN-1193-1947 Effect of product of inertia on lateral stability《惯性积对横向稳定性的影响》.pdf
  • NASA NACA-TN-1197-1947 Some investigations of the general instability of stiffened metal cylinders VIII - stiffened metal cylinders subjected to pure torsion《硬化金属汽缸VIII一般稳定性的一些研究 承.pdf NASA NACA-TN-1197-1947 Some investigations of the general instability of stiffened metal cylinders VIII - stiffened metal cylinders subjected to pure torsion《硬化金属汽缸VIII一般稳定性的一些研究 承.pdf
  • NASA NACA-TN-1212-1947 Effect of reflex camber on the aerodynamic characteristics of a highly tapered moderately swept-back wing at Reynolds numbers up to 8 000 000《当雷诺数为8 000 000时.pdf NASA NACA-TN-1212-1947 Effect of reflex camber on the aerodynamic characteristics of a highly tapered moderately swept-back wing at Reynolds numbers up to 8 000 000《当雷诺数为8 000 000时.pdf
  • NASA NACA-TN-1222-1947 Buckling stresses of simply supported rectangular flat plates in shear《受剪的简支矩形平板和屈曲应力》.pdf NASA NACA-TN-1222-1947 Buckling stresses of simply supported rectangular flat plates in shear《受剪的简支矩形平板和屈曲应力》.pdf
  • NASA NACA-TN-1245-1947 Summary of lateral-control research《横向控制研究的总结》.pdf NASA NACA-TN-1245-1947 Summary of lateral-control research《横向控制研究的总结》.pdf
  • NASA NACA-TN-1248-1947 Wind-tunnel investigation of control-surface characteristics of plain and balanced flaps with several trailing-edge angles on a NACA 0009 tapered semispan wi.pdf NASA NACA-TN-1248-1947 Wind-tunnel investigation of control-surface characteristics of plain and balanced flaps with several trailing-edge angles on a NACA 0009 tapered semispan wi.pdf
  • NASA NACA-TN-1270-1947 Experimental and calculated characteristics of several NACA 44-series wings with aspect ratios of 8 10 and 12 and taper ratios of 2 5 and 3 5《展弦比为8 10和12且锥形比.pdf NASA NACA-TN-1270-1947 Experimental and calculated characteristics of several NACA 44-series wings with aspect ratios of 8 10 and 12 and taper ratios of 2 5 and 3 5《展弦比为8 10和12且锥形比.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