EFFECTS OF BOUNDARY CONDITIONS ON THE STABILITY OF CYLINDERS SUBJECT TO LATERAL AND AXIAL PRESSURES

被引:70
作者
SOBEL, LH
机构
关键词
D O I
10.2514/3.2572
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:1437 / 1440
页数:4
相关论文
共 9 条
  • [1] BATDORF SB, 1947, NACA TR874, P17
  • [2] FORSBERG K, 1964, AIAA6477 PREPR
  • [3] FORSBERG K, UNPUB AIAA J
  • [4] Galletly G.D., 1956, J APPL MECH, V23, P351
  • [5] BUCKLING OF THIN CYLINDRICAL SHELLS SUBJECT TO HYDROSTATIC PRESSURE
    NASH, WA
    [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (05): : 354 - 355
  • [6] PALYI OM, 1958, IZV AKAD NAUK TN JAN, P126
  • [7] SINGER J, 1960, J APPL MECH T AS DEC, P737
  • [8] TITCHMARSH EC, 1939, THEORY FUNCTIONS, P155
  • [9] von Mises R, 1929, KRITISCHE AUSSENDRUC, P418