NF P85-560-1992 Jointing products Glazing materials and compouds for sealing Bedding devices made of flexible cellular materials Specifications 《接缝用品 密封用釉料和化合物 粘滞油基密封剂 柔软蜂窝状材料热垫层 规.pdf

上传人:priceawful190 文档编号:1004211 上传时间:2019-03-18 格式:PDF 页数:3 大小:111.36KB
下载 相关 举报
NF P85-560-1992 Jointing products Glazing materials and compouds for sealing Bedding devices made of flexible cellular materials Specifications 《接缝用品 密封用釉料和化合物 粘滞油基密封剂 柔软蜂窝状材料热垫层 规.pdf_第1页
第1页 / 共3页
NF P85-560-1992 Jointing products Glazing materials and compouds for sealing Bedding devices made of flexible cellular materials Specifications 《接缝用品 密封用釉料和化合物 粘滞油基密封剂 柔软蜂窝状材料热垫层 规.pdf_第2页
第2页 / 共3页
NF P85-560-1992 Jointing products Glazing materials and compouds for sealing Bedding devices made of flexible cellular materials Specifications 《接缝用品 密封用釉料和化合物 粘滞油基密封剂 柔软蜂窝状材料热垫层 规.pdf_第3页
第3页 / 共3页
亲,该文档总共3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-A9B17-1949 Chordwise and spanwise loadings measured at low speed on large triangular wings《在低速时测量大三角形机翼弦向和顺翼展方向的荷载》.pdf NASA NACA-RM-A9B17-1949 Chordwise and spanwise loadings measured at low speed on large triangular wings《在低速时测量大三角形机翼弦向和顺翼展方向的荷载》.pdf
  • NASA NACA-RM-A9C21-1949 Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees  effects of split flaps elevons and leading-edge devices at low spee.pdf NASA NACA-RM-A9C21-1949 Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees effects of split flaps elevons and leading-edge devices at low spee.pdf
  • NASA NACA-RM-A9F16-1949 A comparison of two submerged inlets at subsonic and transonic speeds《在亚音速和跨音速时两个嵌入式进气道的对比》.pdf NASA NACA-RM-A9F16-1949 A comparison of two submerged inlets at subsonic and transonic speeds《在亚音速和跨音速时两个嵌入式进气道的对比》.pdf
  • NASA NACA-RM-E50D05-1950 Experimental investigation of supersonic flow with detached shock waves for Mach numbers between 1 8 and 2 9《在马赫数为1 8至2 9时 带有脱体激波的超音速流动的实验研究》.pdf NASA NACA-RM-E50D05-1950 Experimental investigation of supersonic flow with detached shock waves for Mach numbers between 1 8 and 2 9《在马赫数为1 8至2 9时 带有脱体激波的超音速流动的实验研究》.pdf
  • NASA NACA-RM-E50H23-1950 Correlation of forced-convection heat-transfer data for air flowing in smooth platinum tube with long-approach entrance at high surface and inlet-air tempe.pdf NASA NACA-RM-E50H23-1950 Correlation of forced-convection heat-transfer data for air flowing in smooth platinum tube with long-approach entrance at high surface and inlet-air tempe.pdf
  • NASA NACA-RM-E51A25-1951 Investigation of altitude ignition acceleration and steady-state operation with single combustor of J47 turbojet engine《带有J47涡轮喷气发动机的单一燃烧器高度点火 加速和稳态操作的研究》.pdf NASA NACA-RM-E51A25-1951 Investigation of altitude ignition acceleration and steady-state operation with single combustor of J47 turbojet engine《带有J47涡轮喷气发动机的单一燃烧器高度点火 加速和稳态操作的研究》.pdf
  • NASA NACA-RM-E51C06-1951 Aerodynamic characteristics of four bodies of revolution showing some effects of afterbody shape and fineness ratio at free-stream Mach numbers from 1 50 t.pdf NASA NACA-RM-E51C06-1951 Aerodynamic characteristics of four bodies of revolution showing some effects of afterbody shape and fineness ratio at free-stream Mach numbers from 1 50 t.pdf
  • NASA NACA-RM-E51H13-1951 Aerodynamics of slender bodies at Mach number of 3 12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) I - body of revolution with near-parabolic .pdf NASA NACA-RM-E51H13-1951 Aerodynamics of slender bodies at Mach number of 3 12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) I - body of revolution with near-parabolic .pdf
  • NASA NACA-RM-E51J23-1951 Generalization of turbojet and turbine-propeller engine performance in windmilling condition《在螺旋桨自转情况下涡轮喷气飞机和涡轮螺旋桨发动机的性能概括》.pdf NASA NACA-RM-E51J23-1951 Generalization of turbojet and turbine-propeller engine performance in windmilling condition《在螺旋桨自转情况下涡轮喷气飞机和涡轮螺旋桨发动机的性能概括》.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