NBN T 04-290-1985 5000 Phenoland cresols for industrial use - Determination of crystallizing point after drying with a molecular sieve《工业用苯酚 使用分子筛干燥后结晶点的测定》.pdf

上传人:eastlab115 文档编号:988558 上传时间:2019-03-15 格式:PDF 页数:1 大小:42.39KB
下载 相关 举报
NBN T 04-290-1985 5000 Phenoland cresols for industrial use - Determination of crystallizing point after drying with a molecular sieve《工业用苯酚 使用分子筛干燥后结晶点的测定》.pdf_第1页
第1页 / 共1页
亲,该文档总共1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-RM-L51L10-1952 Wind-tunnel investigation at high subsonic speeds of spoilers of large projection on an NACA 65A006 wing with quarter-chord line swept back 32 6 degrees《在高.pdf NASA NACA-RM-L51L10-1952 Wind-tunnel investigation at high subsonic speeds of spoilers of large projection on an NACA 65A006 wing with quarter-chord line swept back 32 6 degrees《在高.pdf
  • NASA NACA-RM-L52A23-1952 Preliminary investigation at transonic speeds of the effect of balancing tabs on the hinge-moment and other aerodynamic characteristics of a full-span flappect.pdf NASA NACA-RM-L52A23-1952 Preliminary investigation at transonic speeds of the effect of balancing tabs on the hinge-moment and other aerodynamic characteristics of a full-span flappect.pdf
  • NASA NACA-RM-L52A29-1952 Wind-tunnel investigation of the aerodynamic characteristics in pitch of wing-fuselage combinations at high subsonic speeds aspect-ratio series《在高亚音速展弦比系列下.pdf NASA NACA-RM-L52A29-1952 Wind-tunnel investigation of the aerodynamic characteristics in pitch of wing-fuselage combinations at high subsonic speeds aspect-ratio series《在高亚音速展弦比系列下.pdf
  • NASA NACA-RM-L52B13-1952 Effects of some primary variables of rectangular vortex generators on the static-pressure rise through a short diffuser《矩形旋涡发生器的一些初级变量对通过短扩散器静态压力上升的影响》.pdf NASA NACA-RM-L52B13-1952 Effects of some primary variables of rectangular vortex generators on the static-pressure rise through a short diffuser《矩形旋涡发生器的一些初级变量对通过短扩散器静态压力上升的影响》.pdf
  • NASA NACA-RM-L52C11-1952 Low-speed longitudinal aerodynamic characteristics of a twisted and cambered wing of 45 degrees sweepback and aspect ratio 8 with and without high-lift andolds.pdf NASA NACA-RM-L52C11-1952 Low-speed longitudinal aerodynamic characteristics of a twisted and cambered wing of 45 degrees sweepback and aspect ratio 8 with and without high-lift andolds.pdf
  • NASA NACA-RM-L52E02-1952 Longitudinal frequency-response and stability characteristics of the Douglas D-558-II airplane as determined from transient response to a Mach number of 0 .pdf NASA NACA-RM-L52E02-1952 Longitudinal frequency-response and stability characteristics of the Douglas D-558-II airplane as determined from transient response to a Mach number of 0 .pdf
  • NASA NACA-RM-L52E06-1952 Effects of stabilizing fins and a rear-support sting on the base pressure of a body of revolution in free flight at Mach numbers from 0 7 to 1 3《当马赫数为0 7至1.pdf NASA NACA-RM-L52E06-1952 Effects of stabilizing fins and a rear-support sting on the base pressure of a body of revolution in free flight at Mach numbers from 0 7 to 1 3《当马赫数为0 7至1.pdf
  • NASA NACA-RM-L52G07-1952 Wind-tunnel investigation of the low-speed static and rotary stability derivatives of a 0 13-scale model of the Douglas D-558-II airplane in the landing co.pdf NASA NACA-RM-L52G07-1952 Wind-tunnel investigation of the low-speed static and rotary stability derivatives of a 0 13-scale model of the Douglas D-558-II airplane in the landing co.pdf
  • NASA NACA-RM-L52G18-1952 Investigation of the effects of variations in the Reynolds number between 0 4 x 10(exp 6) and 3 0 x 10(exp 6) on the low-speed aerodynamic characteristics ith .pdf NASA NACA-RM-L52G18-1952 Investigation of the effects of variations in the Reynolds number between 0 4 x 10(exp 6) and 3 0 x 10(exp 6) on the low-speed aerodynamic characteristics ith .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