收藏
下载资源 加入VIP,免费下载

NAVY MS28916 NOTICE 1-1996 LIGHT CABIN DOME AIRCRAFT《飞机坐舱顶灯》.pdf

上传人：bonesoil321 文档编号：983898 上传时间：2019-03-12 格式：PDF 页数：1 大小：28.17KB
下载 相关 举报
NAVY MS28916 NOTICE 1-1996 LIGHT CABIN DOME AIRCRAFT《飞机坐舱顶灯》.pdf_第1页
第1页 / 共1页
亲，该文档总共1页，全部预览完了，如果喜欢就下载吧！
资源描述

NOTICE OF INACTIVATION FOR NEW DESIGN MILITARY STANDARD -1 LIGHT, CABIN DOME, AIRCRAFT This notice should be filed in front of MS28916, dated 27 July 1964. MS28916 is inactive for new design and is no longer used, except for replacement purposes. Custodians: Navy - AS Air Force - 99 Preparing activity: Navy - AS (Project 6220- 1 100) Review activity: DLA - GS AMSC NIA FSC 6220 DISTRIBUTION STATEMENT A. .Approved for public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

展开阅读全文
相关资源
猜你喜欢
  • NASA NACA-RM-A51B21-1951 Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 2 triangular wing and an all-movable horizontal tail longit.pdf NASA NACA-RM-A51B21-1951 Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 2 triangular wing and an all-movable horizontal tail longit.pdf
  • NASA NACA-RM-A51C14-1951 A semi-empirical method for calculating the pitching moment of bodies of revolution at low Mach numbers《在低马赫数时回转体俯仰力矩的半经验计算方法》.pdf NASA NACA-RM-A51C14-1951 A semi-empirical method for calculating the pitching moment of bodies of revolution at low Mach numbers《在低马赫数时回转体俯仰力矩的半经验计算方法》.pdf
  • NASA NACA-RM-A51D02-1951 Investigation in the Ames 12-foot pressure wind tunnel of a model horizontal tail of aspect ratio 3 and taper ratio 0 5 having the quarter-chord line swept.pdf NASA NACA-RM-A51D02-1951 Investigation in the Ames 12-foot pressure wind tunnel of a model horizontal tail of aspect ratio 3 and taper ratio 0 5 having the quarter-chord line swept.pdf
  • NASA NACA-RM-A51D25-1951 Low-speed characteristics of a wing having 63 degrees sweepback and uniform camber《带有63后掠角和均匀弧度的机翼低速特性》.pdf NASA NACA-RM-A51D25-1951 Low-speed characteristics of a wing having 63 degrees sweepback and uniform camber《带有63后掠角和均匀弧度的机翼低速特性》.pdf
  • NASA NACA-RM-A51D27-1951 Characteristics throughout the subsonic speed range of a plane wing and of a cambered and twisted wing both having 45 degrees of sweepback《拱形和扭转机翼的飞机机翼(均有4.pdf NASA NACA-RM-A51D27-1951 Characteristics throughout the subsonic speed range of a plane wing and of a cambered and twisted wing both having 45 degrees of sweepback《拱形和扭转机翼的飞机机翼(均有4.pdf
  • NASA NACA-RM-A51G31-1951 The forces and pressure distribution at subsonic speeds on a plane wing having 45 degrees of sweepback an aspect ratio of 3 and a taper ratio of 0 5《在亚音速下 .pdf NASA NACA-RM-A51G31-1951 The forces and pressure distribution at subsonic speeds on a plane wing having 45 degrees of sweepback an aspect ratio of 3 and a taper ratio of 0 5《在亚音速下 .pdf
  • NASA NACA-RM-A51H02-1951 Lift drag and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds - plane triangular wing of aspect ratio 3 with NACA 0003-63 secti.pdf NASA NACA-RM-A51H02-1951 Lift drag and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds - plane triangular wing of aspect ratio 3 with NACA 0003-63 secti.pdf
  • NASA NACA-RM-A51J11-1951 The effects at transonic speeds of thickening the trailing edge of a wing with a 4-percent-thick circular-arc airfoil《在跨音速下 将带有4%厚度圆弧机翼的机翼后缘增厚的效果》.pdf NASA NACA-RM-A51J11-1951 The effects at transonic speeds of thickening the trailing edge of a wing with a 4-percent-thick circular-arc airfoil《在跨音速下 将带有4%厚度圆弧机翼的机翼后缘增厚的效果》.pdf
  • NASA NACA-RM-A51L03-1952 Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 2 triangular wing and an all-movable horizontal tail latera.pdf NASA NACA-RM-A51L03-1952 Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 2 triangular wing and an all-movable horizontal tail latera.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