JIS Z 9110-2010 0625 General rules of recommended lighting levels《照明度推荐性通用规则》.pdf

相关资源

JIS C9901 AMD 1-2018 Methods of calculation and representation of energy efficiency standard achievement percentage of electrical and electronic appliances (Ame.pdf

JIS B8366-1-2018 Fluid power systems and components -- Cylinders 《流体动力系统和元件 液压缸 元件和识别代码 第1部分 缸径和活塞杆.pdf

JIS Z4716-2018 Measurement methods of leakage X-ray from X-ray examination rooms《X射线检查室泄漏X射线的测量方法》.pdf

JIS Z2345-4-2018 Standard test blocks for ultrasonic testing -- Part 4 Standard test blocks for angle beam ultrasonic testing《超声检测用标准试块 第4部分 斜射超声检测用标准试块》.pdf

JIS Z2345-3-2018 Standard test blocks for ultrasonic testing -- Part 3 Standard test blocks for normal ultrasonic testing《超声检测用标准试块 第3部分 普通超声检测用标准试块》.pdf

JIS Z2345-2-2018 Standard test blocks for ultrasonic testing -- Part 2 A7963 Standard Test Block《超声检测用标准试块 第2部分 A7963标准试块》.pdf

JIS Z2345-1-2018 Standard test blocks for ultrasonic testing -- Part 1 A1 Standard Test Block《超声检测用标准试块 第1部分 A1标准试块》.pdf

JIS Z2242-2018 Method for Charpy pendulum impact test of metallic materials《金属材料的摆式冲击试验方法》.pdf

JIS Z0150-2018 Packaging -- Distiribution packaging -- Graphical symbols for handling and storage of packages《包装 畸变包装 包装处理和储存用图形符号》.pdf

JIS X6302-9-2018 Identification cards -- Recording technique -- Part 9 Tactile identifier mark《识别卡 记录技术 第9部分 触式鉴别器标志》.pdf

猜你喜欢

NASA NACA-RM-A7K03-1948 Low-speed investigation of a small triangular wing of aspect ratio 2 0 I the effect of combination with a body revolution and height above a ground plane《展.pdf

NASA NACA-RM-A7K24-1948 Wind-tunnel investigation of horizontal tails I - unswept and 35 degrees swept-back plan forms of aspect ratio 3《水平尾翼的风洞研究 I 展弦比为3的非后掠翼且后掠角为35的平面图》.pdf

NASA NACA-RM-A7K28-1948 High-speed stability and control characteristics of a fighter airplane model with a swept-back wing and tail《带有后掠翼和尾翼的战斗机模型的高速稳定性和控制特性》.pdf

NASA NACA-RM-A7L02-1948 A summary and analysis of wind-tunnel data on the lift and hinge-moment characteristics of control surfaces up to a Mach number of 0 90《在马赫数为0 90时 操纵面的升力和铰链.pdf

NASA NACA-RM-A7L11-1948 Low-speed investigation of a small triangular wing of aspect ratio 2 0 II flaps on flat-plate models《展弦比为2 0的小型三角形机翼的低速研究 II 平坦飞机模型的襟翼》.pdf

NASA NACA-RM-A7L16-1948 A WIND-TUNNEL INVESTIGATION AT LOW SPEED OF VARIOUS LATERAL CONTROLS ON A 45 SWEPT-BACK WING《在各种横向控制低速下45后掠翼的风洞研究》.pdf

NASA NACA-RM-A8A20-1948 An investigation of submerged air inlets on a 1 4-scale model of a typical fighter-type airplane《嵌入式进气道在典型战斗机的1 4比例模型上的研究》.pdf

NASA NACA-RM-A8B11-1948 Wind-tunnel investigation of horizontal tails II - unswept and 35 degrees swept-back plan forms of aspect ratio 4 5《水平尾翼的风洞研究 II 展弦比为4 5的非后掠翼且后掠角为35的平面图》.pdf

NASA NACA-RM-A8C03-1948 Low-speed investigation of a small triangular wing of aspect ratio 2 0 III - static stability with twin vertical fins《展弦比为2 0的小型三角形机翼的低速研究 III 双垂尾的静态稳定性》.pdf