NBN C 32-124 ADD 2-1984 1875 《装置绝缘导线和电缆，国有类型 聚氯乙烯绝缘电缆和导体，名义电压Uo U 低于》.pdf

相关资源

JIS K6876-2-2007 塑料.丙烯腈-苯乙烯-丙烯酸酯(ASA)、丙烯腈-(乙烯-丙烯-二烯烃)-苯乙烯(AEPDS)和丙烯腈-(聚氯乙烯)-苯乙烯.pdf

JIS A4714-1995 硬质聚氯乙烯内窗窗框.pdf

JIS A5702-1993 硬质聚氯乙烯波纹板.pdf

QB T 2029-1994 丙烯腈-丁二烯-苯乙烯聚氯乙烯(ABSPVC)片材.pdf

JIS C3316-2000 电气设备用聚氯乙烯绝缘线.pdf

JIS A5705-2005 地板覆盖物 聚氯乙烯.pdf

JB T 7630.3-1998 铅酸蓄电池烧结聚氯乙烯隔板.pdf

JIS K6734-2000 塑料.未增塑的聚氯乙烯板.pdf

JIS K6743-2007 输水用硬质聚氯乙烯管接头.pdf

JIS K6777-2009 冷热水供水系统用氯化聚氯乙烯(PVC-C)管道配件(追補1).pdf

猜你喜欢

NASA NACA-RM-L58B05-1958 Low-subsonic investigation to determine the chordwise pressure distribution and effectiveness of spoilers on a thin low-aspect-ratio unswept untapered semiaili.pdf

NASA NACA-RM-L58C18-1958 Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach n.pdf

NASA NACA-RM-L6L27-1947 Effects of a fuselage and various high-lift and stall-control flaps on aerodynamic characteristics in pitch of an NACA 64-series 40 degrees swept-back wing《.pdf

NASA NACA-RM-L7A30-1947 Wind-tunnel investigation of air loads over a double slotted flap on the NACA 65(216)-215 a = 0 8 airfoil section《NACA 65(216)-215 a = 0 8翼剖面上双开缝襟翼空气荷载的风洞研究.pdf

NASA NACA-RM-L7C11-1947 Aerodynamic characteristics of a 45 degrees swept-back wing with aspect ratio of 3 5 and NACA 2S-50(05)-50(05) airfoil sections《展弦比为3 5且带有NACA 2S-50(05)-50(.pdf

NASA NACA-RM-L7D08-1947 Pressure-distribution measurements on a full-scale horizontal tail surface for a Mach number range of 0 20 to 0 70《当马赫数为0 20至0 70时 全比例水平尾翼面上压力分布的测量》.pdf

NASA NACA-RM-L7D11-1947 Wind-tunnel investigation of bomb-bay configurations intended to minimize the tumbling of light-weight bombs《旨在使轻质炸弹的歪斜最小化的炸弹湾结构的风洞研究》.pdf

NASA NACA-RM-L7E13-1947 Effects of a Fuselage on the Aerodynamic Characteristics of a 42 Degrees Sweptback Wing at Reynolds Numbers to 8 000 000《当雷诺数为8 000 000时 机身对42后掠翼空气动力特性的影响》.pdf

NASA NACA-RM-L7G09-1947 Investigation of high-lift and stall-control devices on a NACA 64-series 42 degrees sweptback wing with and without fuselage《带有或不带机身的NACA第64系列42后掠翼上高升力和失速控制.pdf