2015年西北师范大学821程序设计与数据结构考研真题.pdf

上传人:proposalcash356 文档编号:1267371 上传时间:2019-09-07 格式:PDF 页数:8 大小:1.30MB
下载 相关 举报
2015年西北师范大学821程序设计与数据结构考研真题.pdf_第1页
第1页 / 共8页
2015年西北师范大学821程序设计与数据结构考研真题.pdf_第2页
第2页 / 共8页
2015年西北师范大学821程序设计与数据结构考研真题.pdf_第3页
第3页 / 共8页
2015年西北师范大学821程序设计与数据结构考研真题.pdf_第4页
第4页 / 共8页
2015年西北师范大学821程序设计与数据结构考研真题.pdf_第5页
第5页 / 共8页
点击查看更多>>
资源描述
展开阅读全文
相关资源
猜你喜欢
  • NASA-TM-87659-1986 Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate《在平板中带有多种长度深度比的矩形箱子空腔超音速轴向力量特性》.pdf NASA-TM-87659-1986 Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate《在平板中带有多种长度深度比的矩形箱子空腔超音速轴向力量特性》.pdf
  • NASA-TM-88361-1987 Interaction between a vortex and a turbulent boundary layer - Part I Mean flow evolution and turbulence properties《涡流和混乱边界层之间的互相作用 第I部分 平均流量演变和湍流性能》.pdf NASA-TM-88361-1987 Interaction between a vortex and a turbulent boundary layer - Part I Mean flow evolution and turbulence properties《涡流和混乱边界层之间的互相作用 第I部分 平均流量演变和湍流性能》.pdf
  • NASA-TM-X-1517-1968 Effect of boattail juncture shape on pressure drag coefficients of isolated afterbodies《船形尾部接缝形状对绝缘飞机后体压力阻力系数的影响》.pdf NASA-TM-X-1517-1968 Effect of boattail juncture shape on pressure drag coefficients of isolated afterbodies《船形尾部接缝形状对绝缘飞机后体压力阻力系数的影响》.pdf
  • NASA-TM-X-1658-1968 Aerodynamic characteristics of bodies of revolution at Mach numbers from 1 50 to 2 86 and angles of attack to 180 deg《当马赫数为1 50至2 86且攻角为180时 回转体的空气动力特性》.pdf NASA-TM-X-1658-1968 Aerodynamic characteristics of bodies of revolution at Mach numbers from 1 50 to 2 86 and angles of attack to 180 deg《当马赫数为1 50至2 86且攻角为180时 回转体的空气动力特性》.pdf
  • NASA-TM-X-1931-1969 Loss of forced cooling flow in the Plum Brook Reactor《在上等布鲁克反应器中的强制冷却流量损失》.pdf NASA-TM-X-1931-1969 Loss of forced cooling flow in the Plum Brook Reactor《在上等布鲁克反应器中的强制冷却流量损失》.pdf
  • NASA-TM-X-1958-1970 Comparison of experimental and ideal leakage flows through labyrinth seals for very small pressure differences《通过很小压差的迷宫式密封对实验性和理想漏流进行对比》.pdf NASA-TM-X-1958-1970 Comparison of experimental and ideal leakage flows through labyrinth seals for very small pressure differences《通过很小压差的迷宫式密封对实验性和理想漏流进行对比》.pdf
  • NASA-TM-X-213-1960 Investigation of the aerodynamic characteristics of a supersonic horizontal- attitude VTOL airplane model at Mach numbers of 1 57 2 14 2 54 and 2 87《当马赫数为1 57 2 .pdf NASA-TM-X-213-1960 Investigation of the aerodynamic characteristics of a supersonic horizontal- attitude VTOL airplane model at Mach numbers of 1 57 2 14 2 54 and 2 87《当马赫数为1 57 2 .pdf
  • NASA-TM-X-2163-1971 Some transonic and supersonic dynamic stability characteristics of a variable-sweep-wing tactical fighter model《可变掠翼战术战斗机模型的一些跨音速和超音速动态稳定特性》.pdf NASA-TM-X-2163-1971 Some transonic and supersonic dynamic stability characteristics of a variable-sweep-wing tactical fighter model《可变掠翼战术战斗机模型的一些跨音速和超音速动态稳定特性》.pdf
  • NASA-TM-X-2284-1971 Stability and control characteristics at Mach numbers 1 60 to 2 86 of a variable-sweep fighter configuration with supercritical airfoil sections《当马赫数为1 60至2 86时.pdf NASA-TM-X-2284-1971 Stability and control characteristics at Mach numbers 1 60 to 2 86 of a variable-sweep fighter configuration with supercritical airfoil sections《当马赫数为1 60至2 86时.pdf
  • 相关搜索
    资源标签

    当前位置:首页 > 考试资料 > 大学考试

    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