搜索
麦多课文库
收藏
下载资源
加入VIP,免费下载
SNI 2929-2008 《用于内燃机的火花塞》.pdf
上传人:
outsidejudge265
文档编号:1051225
上传时间:2019-03-27
格式:PDF
页数:19
大小:1.13MB
下载
相关
举报
第1页 / 共19页
第2页 / 共19页
第3页 / 共19页
第4页 / 共19页
第5页 / 共19页
点击查看更多>>
资源描述
展开
阅读全文
相关资源
STAS 5015-1955 《火花塞插头》.pdf
GB T 7825-1987 火花塞.pdf
SAE J 548-1987 Spark Plugs《火花塞》.pdf
SNI 09-2656-1992 Spark plugs《火花塞》.pdf
GB T 20714-2006 火花塞接线端子.pdf
GB T 2900.9-1994 电工术语 火花塞.pdf
GB T 2900.9-1994 电工术语 火花塞.pdf
JB T 6472-1992 电阻型火花塞.pdf
SAE ARP 368C-1972 Spark Plug Thread Form Data (60 Degrees Thread Angle)《火花塞螺纹型数据(60螺纹角)》.pdf
SAE AS 889-1966 Calibration Spark Plugs《校准火花塞》.pdf
猜你喜欢
NASA NACA-RM-A53J23-1954 The effects of operating propellers on the longitudinal characteristics at high subsonic speeds of a four-engine tractor airplane configuration having a wi rat.pdf
NASA NACA-RM-A53L22-1954 An experimental investigation of four triangular-wing-body combinations in sideslip at Mach numbers 0 6 0 9 1 4 and 1 7《在马赫数为0 6 0 9 1 4和1 7时 侧滑中四个三角形机翼组合的.pdf
NASA NACA-RM-A54B08-1954 The effect of lip shape on a nose-inlet installation at Mach numbers from 0 to 1 5 and a method for optimizing engine-inlet combinations《在马赫数为0-1 5时 唇形对头部进.pdf
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
相关搜索
SNI29292008
用于
内燃机
火花塞
PDF
资源标签
火花塞螺纹
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