SIS SMS 2357-1969 Hydraulic cylinders tu bes《液压缸管》.pdf

上传人:rimleave225 文档编号:1038713 上传时间:2019-03-24 格式:PDF 页数:4 大小:139.44KB
下载 相关 举报
SIS SMS 2357-1969 Hydraulic cylinders tu bes《液压缸管》.pdf_第1页
第1页 / 共4页
SIS SMS 2357-1969 Hydraulic cylinders tu bes《液压缸管》.pdf_第2页
第2页 / 共4页
SIS SMS 2357-1969 Hydraulic cylinders tu bes《液压缸管》.pdf_第3页
第3页 / 共4页
SIS SMS 2357-1969 Hydraulic cylinders tu bes《液压缸管》.pdf_第4页
第4页 / 共4页
亲,该文档总共4页,全部预览完了,如果喜欢就下载吧!
资源描述
展开阅读全文
相关资源
猜你喜欢
  • 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-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-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-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-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-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-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-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 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
  • NASA NACA-RM-L7G31-1947 Lateral stability and control characteristics of an airplane model having 42 8 degrees sweptback circular-arc wing with aspect ratio 4 00 taper ratio 0 50 a.pdf NASA NACA-RM-L7G31-1947 Lateral stability and control characteristics of an airplane model having 42 8 degrees sweptback circular-arc wing with aspect ratio 4 00 taper ratio 0 50 a.pdf
  • 相关搜索

    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