DB65 T 3973-2017 德国肉用美利奴种羊.pdf

上传人:testyield361 文档编号:1495795 上传时间:2020-11-01 格式:PDF 页数:5 大小:894.68KB
下载 相关 举报
DB65 T 3973-2017 德国肉用美利奴种羊.pdf_第1页
第1页 / 共5页
DB65 T 3973-2017 德国肉用美利奴种羊.pdf_第2页
第2页 / 共5页
DB65 T 3973-2017 德国肉用美利奴种羊.pdf_第3页
第3页 / 共5页
DB65 T 3973-2017 德国肉用美利奴种羊.pdf_第4页
第4页 / 共5页
DB65 T 3973-2017 德国肉用美利奴种羊.pdf_第5页
第5页 / 共5页
亲,该文档总共5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-L9A07-1949 Low-speed investigation of aileron and spoiler characteristics of a wing having 42 degrees sweepback of the leading edge and circular-arc airfoil sections aexp .pdf NASA NACA-RM-L9A07-1949 Low-speed investigation of aileron and spoiler characteristics of a wing having 42 degrees sweepback of the leading edge and circular-arc airfoil sections aexp .pdf
  • NASA NACA-RM-L9B02-1949 Full-scale investigation of a wing with the leading edge swept back 47 5 degrees and having circular-arc and finite-trailing-edge-thickness ailerons《带有前缘47 .pdf NASA NACA-RM-L9B02-1949 Full-scale investigation of a wing with the leading edge swept back 47 5 degrees and having circular-arc and finite-trailing-edge-thickness ailerons《带有前缘47 .pdf
  • NASA NACA-RM-L9D06-1949 Wing-tunnel investigation at high subsonic speeds of the lateral-control characteristics of an aileron and a stepped spoiler on a wing with leading edge swe.pdf NASA NACA-RM-L9D06-1949 Wing-tunnel investigation at high subsonic speeds of the lateral-control characteristics of an aileron and a stepped spoiler on a wing with leading edge swe.pdf
  • NASA NACA-RM-L9E02-1949 The effect of span and deflection of split flaps and leading-edge roughness on the longitudinal stability and gliding characteristics of a 42 degrees sweptb襟.pdf NASA NACA-RM-L9E02-1949 The effect of span and deflection of split flaps and leading-edge roughness on the longitudinal stability and gliding characteristics of a 42 degrees sweptb襟.pdf
  • NASA NACA-RM-L9E10-1949 Effects of Mach number and sweep on the damping-in-roll characteristics of wings of aspect ratio 4《马赫数和扫掠对展弦比为4的机翼滚转阻尼特性的影响》.pdf NASA NACA-RM-L9E10-1949 Effects of Mach number and sweep on the damping-in-roll characteristics of wings of aspect ratio 4《马赫数和扫掠对展弦比为4的机翼滚转阻尼特性的影响》.pdf
  • NASA NACA-RM-L9E24-1949 Investigation of low-speed aileron control characteristics at a Reynolds number of 6 800 000 of a wing with leading edge swept back 42 degrees with and with.pdf NASA NACA-RM-L9E24-1949 Investigation of low-speed aileron control characteristics at a Reynolds number of 6 800 000 of a wing with leading edge swept back 42 degrees with and with.pdf
  • NASA NACA-RM-L9F14-1949 Effect of sweepback on the low-speed static and rolling stability derivatives of thin tapered wings of aspect ratio 4《后掠角对展弦比为4的薄锥形机翼低速静态和旋转稳定性导数的影响》.pdf NASA NACA-RM-L9F14-1949 Effect of sweepback on the low-speed static and rolling stability derivatives of thin tapered wings of aspect ratio 4《后掠角对展弦比为4的薄锥形机翼低速静态和旋转稳定性导数的影响》.pdf
  • NASA NACA-RM-L9J04-1949 Effect of airfoil section and tip tanks on the aerodynamic characteristics at high subsonic speeds of an unswept wing of aspect ratio 5 16 and taper ratio 0.pdf NASA NACA-RM-L9J04-1949 Effect of airfoil section and tip tanks on the aerodynamic characteristics at high subsonic speeds of an unswept wing of aspect ratio 5 16 and taper ratio 0.pdf
  • NASA NACA-RM-L9K11-1950 Measurements of aerodynamic characteristics of a 35 degrees sweptback NACA 65-009 airfoil model with 1 4-chord bevelled-trailing-edge flap and trim tab by t.pdf NASA NACA-RM-L9K11-1950 Measurements of aerodynamic characteristics of a 35 degrees sweptback NACA 65-009 airfoil model with 1 4-chord bevelled-trailing-edge flap and trim tab by t.pdf
  • 相关搜索
    资源标签

    当前位置:首页 > 标准规范 > 地方标准

    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