搜索
麦多课文库
收藏
下载资源
加入VIP,免费下载
SNI 19-1935-1990 Main entry (cataloguing rules)《主要索引(编写目录规则)》.pdf
上传人:
confusegate185
文档编号:1050912
上传时间:2019-03-27
格式:PDF
页数:33
大小:1.26MB
下载
相关
举报
第1页 / 共33页
第2页 / 共33页
第3页 / 共33页
第4页 / 共33页
第5页 / 共33页
点击查看更多>>
资源描述
展开
阅读全文
相关资源
IRS 70778-2-2018 Recommendations for determining the carrying capacity and fatigue risks of existing metallic railway bridges.pdf
IRS 70712-2018 Rail defects.pdf
IRS 50596-6-2018 Conditions for coding intermodal loading units in combined transport combined transport lines and wagons.pdf
IRS 50596-5-2018 Transport of road vehicles on wagons-Technical Organisation-Conveyance of semi-trailers with P coding or N coding on recess wagons.pdf
IESNA TM-23-2017 Lighting Control Protocols.pdf
IESNA RP-2-2017 Recommended Practice for Retail Lighting.pdf
ITU-R RAPPORT M 766-2 FRENCH-1990 Feasibility of frequency sharing between the GPS and other services《全球定位系统和其他服务之间的频率共享的可行性》.pdf
ITU-R RAPPORT M 763-3 FRENCH-1990 Signal level variation due to multipath effects and blockage by ship-s superstructure in maritime mobile-satellite service lin.pdf
ITU-R RAPPORT M 739-1 FRENCH-1986 Interference due to intermodulation products in the land mobile service between 25 and 100 MHz《由于互调产物在陆地移动服务25和100 MHz之间产生的干扰》.pdf
ITU-R RAPPORT M 319-7 FRENCH-1990 Characteristics of equipment and principles governing the assignment of frequency channels between 25 and 100 MHz for land mob.pdf
猜你喜欢
NASA NACA-RM-A54D19-1954 Pressure distributions on triangular and rectangular wings to high angles of attack - Mach numbers 1 45 and 1 97《在马赫数为1 45和1 97时 三角形和矩形机翼的高攻角压力分布》.pdf
NASA NACA-RM-A54D22-1954 Investigation of the normal force accompanying thrust-axis inclination of the NACA 1 167-(0)(03)-058 and the NACA 1 167-(0)(05)-058 three-blade propellers .pdf
NASA NACA-RM-A54F18-1954 A comparison of the longitudinal aerodynamic characteristics at mach numbers up to 0 94 of sweptback wings having NACA 4-digit or NACA 64A thickness distri.pdf
NASA NACA-RM-A54J12-1955 Pressure distributions on triangular and rectangular wings to high angles of attack - Mach numbers 2 46 and 3 36《当马赫数达为2 46和3 36时 三角形和矩形机翼大攻角上的压力分布》.pdf
NASA NACA-RM-A54J19-1955 Application of wing-body theory to drag reduction at low supersonic speeds《在低超声速时 翼身原理对减阻的应用》.pdf
NASA NACA-RM-A54J20-1955 Effect of taper ratio on lift drag and pitching-moment characteristics of thin wings of aspect ratio 3 with 53 1 degrees sweepback of leading edge at subso.pdf
NASA NACA-RM-A55A28-1955 Wind-tunnel measurements at subsonic speeds of the static and dynamic-rotary stability derivatives of a triangular-wing airplane model having a triangular .pdf
NASA NACA-RM-A55D11-1955 Investigation of the effects of an airfoil section modification on the aerodynamic characteristics at subsonic and supersonic speeds of a thin swept wing o亚音.pdf
NASA NACA-RM-A55G19-1955 A study of conical camber for triangular and sweptback wings《三角形和后掠型机翼的锥形弯度研究》.pdf
相关搜索
SNI1919351990MAINENTRYCATALOGUINGRU
主要
索引
编写
目录
规则
PDF
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
登录
首页
资源分类
专题
通知公告