WS T 813-2023 手术部位标识标准.pdf

上传人:terrorscript155 文档编号:1539288 上传时间:2024-02-16 格式:PDF 页数:8 大小:1.48MB
下载 相关 举报
WS T 813-2023 手术部位标识标准.pdf_第1页
第1页 / 共8页
WS T 813-2023 手术部位标识标准.pdf_第2页
第2页 / 共8页
WS T 813-2023 手术部位标识标准.pdf_第3页
第3页 / 共8页
WS T 813-2023 手术部位标识标准.pdf_第4页
第4页 / 共8页
WS T 813-2023 手术部位标识标准.pdf_第5页
第5页 / 共8页
亲,该文档总共8页,到这儿已超出免费预览范围,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-L7K07-1948 Flight characteristics at low speed of delta-wing models《三角形机翼模型低速时的飞行特性》.pdf NASA NACA-RM-L7K07-1948 Flight characteristics at low speed of delta-wing models《三角形机翼模型低速时的飞行特性》.pdf
  • NASA NACA-RM-L8D06-1948 Effect of high-lift devices on the longitudinal and lateral characteristics of a 45 degrees sweptback wing with symmetrical circular-arc sections《高升力装置对带有对称.pdf NASA NACA-RM-L8D06-1948 Effect of high-lift devices on the longitudinal and lateral characteristics of a 45 degrees sweptback wing with symmetrical circular-arc sections《高升力装置对带有对称.pdf
  • NASA NACA-RM-L8D29-1948 Wind-tunnel investigation of high-lift and stall-control devices on a 37 degrees sweptback wing of aspect ratio 6 at high Reynolds numbers《在高雷诺数下 37后掠翼高升力和失.pdf NASA NACA-RM-L8D29-1948 Wind-tunnel investigation of high-lift and stall-control devices on a 37 degrees sweptback wing of aspect ratio 6 at high Reynolds numbers《在高雷诺数下 37后掠翼高升力和失.pdf
  • NASA NACA-RM-L8D30-1948 Effect of leading-edge high-lift devices and split flaps on the maximum-lift and lateral characteristics of a rectangular wing of aspect ratio 3 4 with circ fro.pdf NASA NACA-RM-L8D30-1948 Effect of leading-edge high-lift devices and split flaps on the maximum-lift and lateral characteristics of a rectangular wing of aspect ratio 3 4 with circ fro.pdf
  • NASA NACA-RM-L8E24-1948 Aerodynamic characteristics of a two-blade NACA 10-(3)(08)-03R propeller《双叶片NACA10-(3)(08)-03R螺旋桨的空气动力特性》.pdf NASA NACA-RM-L8E24-1948 Aerodynamic characteristics of a two-blade NACA 10-(3)(08)-03R propeller《双叶片NACA10-(3)(08)-03R螺旋桨的空气动力特性》.pdf
  • NASA NACA-RM-L8G05-1948 Full-scale investigation of an equilateral triangular wing having 10-percent-thick biconvex airfoil sections《带有10%厚度双凸面的翼剖面的等边三角形机翼的全比例研究》.pdf NASA NACA-RM-L8G05-1948 Full-scale investigation of an equilateral triangular wing having 10-percent-thick biconvex airfoil sections《带有10%厚度双凸面的翼剖面的等边三角形机翼的全比例研究》.pdf
  • NASA NACA-RM-L8I03-1948 The effects of high-lift devices on the low-speed stability characteristics of a tapered 37 5 degree sweptback wing of aspect ratio 3 in straight and rollin.pdf NASA NACA-RM-L8I03-1948 The effects of high-lift devices on the low-speed stability characteristics of a tapered 37 5 degree sweptback wing of aspect ratio 3 in straight and rollin.pdf
  • NASA NACA-RM-L8K19-1949 Wind-tunnel investigation at low speeds of various plug-aileron and lift-flap configurations on a 42 degrees sweptback semispan wing《低速下 42半翼展后掠翼上多种插头副翼和升力襟.pdf NASA NACA-RM-L8K19-1949 Wind-tunnel investigation at low speeds of various plug-aileron and lift-flap configurations on a 42 degrees sweptback semispan wing《低速下 42半翼展后掠翼上多种插头副翼和升力襟.pdf
  • NASA NACA-RM-L8K22-1949 Two-dimensional wind-tunnel investigation of two NACA 6-series airfoils with leading-edge slats《带有前缘缝翼的NACA第6系列机翼的二维风洞研究》.pdf NASA NACA-RM-L8K22-1949 Two-dimensional wind-tunnel investigation of two NACA 6-series airfoils with leading-edge slats《带有前缘缝翼的NACA第6系列机翼的二维风洞研究》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 行业标准 > WS卫生行业

    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