CNS 1789-1966 Magnesium Chloride《化学试药(氯化镁)》.pdf

上传人:sofeeling205 文档编号:1244737 上传时间:2019-08-30 格式:PDF 页数:1 大小:78.08KB
下载 相关 举报
CNS 1789-1966 Magnesium Chloride《化学试药(氯化镁)》.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
展开阅读全文
相关资源
猜你喜欢
  • NASA NACA-TN-1248-1947 Wind-tunnel investigation of control-surface characteristics of plain and balanced flaps with several trailing-edge angles on a NACA 0009 tapered semispan wi.pdf NASA NACA-TN-1248-1947 Wind-tunnel investigation of control-surface characteristics of plain and balanced flaps with several trailing-edge angles on a NACA 0009 tapered semispan wi.pdf
  • NASA NACA-TN-1270-1947 Experimental and calculated characteristics of several NACA 44-series wings with aspect ratios of 8 10 and 12 and taper ratios of 2 5 and 3 5《展弦比为8 10和12且锥形比.pdf NASA NACA-TN-1270-1947 Experimental and calculated characteristics of several NACA 44-series wings with aspect ratios of 8 10 and 12 and taper ratios of 2 5 and 3 5《展弦比为8 10和12且锥形比.pdf
  • NASA NACA-TN-1277-1947 Two-dimensional wind-tunnel investigation of the NACA 64(sub 1)-012 airfoil equipped with two types of leading-edge flap《装配有两种类型前缘襟翼NACA 64(下标1)-012机翼的二维风洞研究.pdf NASA NACA-TN-1277-1947 Two-dimensional wind-tunnel investigation of the NACA 64(sub 1)-012 airfoil equipped with two types of leading-edge flap《装配有两种类型前缘襟翼NACA 64(下标1)-012机翼的二维风洞研究.pdf
  • NASA NACA-TN-1278-1947 Experimental determination of the damping in roll and aileron rolling effectiveness of three wings having 2 degrees 42 degrees and 62 degrees sweepback《带有2 4.pdf NASA NACA-TN-1278-1947 Experimental determination of the damping in roll and aileron rolling effectiveness of three wings having 2 degrees 42 degrees and 62 degrees sweepback《带有2 4.pdf
  • NASA NACA-TN-1291-1947 Collection and analysis of wind-tunnel data on the characteristics of isolated tail surfaces with and without end plates《带有和不带端板绝缘尾翼面特性风洞数据的采集和分析》.pdf NASA NACA-TN-1291-1947 Collection and analysis of wind-tunnel data on the characteristics of isolated tail surfaces with and without end plates《带有和不带端板绝缘尾翼面特性风洞数据的采集和分析》.pdf
  • NASA NACA-TN-1293-1947 Tests of the NACA 64(SUB 1)A212 airfoil section with a slat a double slotted flap and boundary-layer control by suction《带有板条和双开缝襟翼和抽吸边界层控制的NACA 64(下标1)A212翼剖.pdf NASA NACA-TN-1293-1947 Tests of the NACA 64(SUB 1)A212 airfoil section with a slat a double slotted flap and boundary-layer control by suction《带有板条和双开缝襟翼和抽吸边界层控制的NACA 64(下标1)A212翼剖.pdf
  • NASA NACA-TN-1294-1947 Investigation of effect of span spanwise location and chordwise location of spoilers on lateral control characteristics of a tapered wing《扰流板翼展 顺翼展方向的位置弦向位置对.pdf NASA NACA-TN-1294-1947 Investigation of effect of span spanwise location and chordwise location of spoilers on lateral control characteristics of a tapered wing《扰流板翼展 顺翼展方向的位置弦向位置对.pdf
  • NASA NACA-TN-1327-1947 Wind-tunnel investigation of the effect of power and flaps on the static lateral characteristics of a single-engine low-wing airplane model《功率和襟翼对单发动机低机翼飞机模型.pdf NASA NACA-TN-1327-1947 Wind-tunnel investigation of the effect of power and flaps on the static lateral characteristics of a single-engine low-wing airplane model《功率和襟翼对单发动机低机翼飞机模型.pdf
  • NASA NACA-TN-1338-1947 Propeller-efficiency charts for light airplanes《轻型飞机的螺旋桨效率图表》.pdf NASA NACA-TN-1338-1947 Propeller-efficiency charts for light airplanes《轻型飞机的螺旋桨效率图表》.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