SFS 3543-1980 《空气调节设备输送管 稳定性要求和防渗性要求》.pdf

相关资源

JIS E6602-2004 机车车辆用空气调节装置.pdf

JB T 7221-1994 单元式空气调节机组用双进风离心通风机.pdf

JIS C8105-2-19-1999 灯具 第2部分 安全的特殊要求.第19节：空气调节：灯具.pdf

JIS C8105-2-19-2010 灯具 第2部分：安全的特殊要求.第19节：空气调节：灯具(修改件1).pdf

CB-Z 232-1986 水面舰艇空气调节系统设计计算方法.pdf

CB T 3817-1998 船舶干粮库的空气调节与通风设计条件和计算基准.pdf

CB T 3773-1996 船舶机舱集控室的空气调节与通风设计条件和计算基准.pdf

CB T 3774-1996 船舶驾驶室的空气调节与通风设计条件和计算基准.pdf

HG T 20656-1998 化工采暖通风与空气调节详细设计内容和深度的规定.pdf

HG T 20698-2009 化工采暧通风与空气调节设计规范.pdf

猜你喜欢

NASA NACA-TN-4041-1957 The subsonic static aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3 I effects of horizontal-tail location and si.pdf

NASA NACA-TN-4042-1957 The subsonic static aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3 II lateral and directional characteristics《带.pdf

NASA NACA-TN-4044-1957 Ground effects on the longitudinal characteristics of two models with wings having low aspect ratio and pointed tips《带有低展弦比和尖头电极机翼的两个飞机模型纵向特性的地面效应》.pdf

NASA NACA-TN-4050-1957 Studies of structural failure due to acoustic loading《由于声荷载结构损坏的研究》.pdf

NASA NACA-TN-4077-1957 Static longitudinal and lateral stability characteristics at low speed of 45 degrees sweptback-midwing models having wings with an aspect ratio of 2 4 or 6《低.pdf

NASA NACA-TN-4117-1957 Experimental investigation of lift drag and pitching moment of five annular airfoils《五个环形机翼升力 阻力和俯仰力矩的实验研究》.pdf

NASA NACA-TN-4122-1957 External interference effects of flow through static-pressure orifices of an NACA airspeed head at a Mach number of 3《当马赫数为3时 通过NACA空速管静态压力孔口气流的外部干扰效应》.pdf

NASA NACA-TN-4146-1958 Contribution of the wing panels to the forces and moments of supersonic wing-body combinations at combined angles《在联合角度下 翼板对超音速机翼机身组合力量和力矩的促进》.pdf

NASA NACA-TN-4172-1958 Noise survey under static conditions of a turbine-driven full-scale modified supersonic propeller with an advance ratio of 3 2《在静态条件下 对工作状态特性系数为3 2涡轮机驱动全面改良的.pdf