搜索
麦多课文库
收藏
下载资源
加入VIP,免费下载
TIS 2121-2002 Semiconductor devices discrete devices part 8 field effect transistors《半导体器件 分立器件 第8部分 场效应晶体管》.pdf
上传人:
hopesteam270
文档编号:1062329
上传时间:2019-03-31
格式:PDF
页数:69
大小:1.87MB
下载
相关
举报
第1页 / 共69页
第2页 / 共69页
第3页 / 共69页
第4页 / 共69页
第5页 / 共69页
点击查看更多>>
资源描述
展开
阅读全文
相关资源
GB T 18904.2-2002 半导体器件 第12-2部分 光电子器件纤维光学系统或子系统用带尾纤的激光二极管模块空白详细规范.pdf
GB T 18904.3-2002 半导体器件 第12-3部分 光电子器件显示用发光二极管空白详细规范.pdf
JB T 10097-1999 电力半导体器件用管壳.pdf
JB T 10097-2000 电力半导体器件用管壳.pdf
JB T 10501-2005 电力半导体器件用管壳瓷件.pdf
JB T 5835-2005 电力半导体器件用门极组合件.pdf
JB T 5844-1991 电力半导体器件参数符号.pdf
JB T 7621-1994 电力半导体器件工艺用高纯水.pdf
JB T 9684-2000 电力半导体器件用散热器选用导则.pdf
JB T 9687.2-1999 电力半导体器件用钨圆片.pdf
猜你喜欢
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-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-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-L52J17-1956 An investigation at Mach numbers of 1 41 and 2 01 of the aerodynamic characteristics of a swept-wing supersonic bomber configuration《当马赫数为1 41至2 01时 掠翼超音速投.pdf
NASA NACA-RM-L52K06-1952 Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2 05 2 54 and 3 04《当马赫数为2 05 2 54和3 04时 半球形机头的压力分布和压力阻力》.pdf
NASA NACA-RM-L52K19-1952 Aerodynamic characteristics of two delta wings at Mach number 4 04 and correlations of lift and minimum-drag data for delta wings at Mach numbers from 1 62.pdf
NASA NACA-RM-L52K20-1952 Summary of pitch-damping derivatives of complete airplane and missile configurations as measured in flight at transonic and supersonic speeds《根据在跨音速和超音速时在飞.pdf
相关搜索
TIS21212002SEMICONDUCTORDEVICESDISC
半导体器件
分立
器件
部分
场效应
晶体管
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