OPTIMIZATION OF AIRPLANE WING STRUCTURES UNDER LANDING LOADS

被引：5
作者：
RAO, SS
机构：
来源：
COMPUTERS & STRUCTURES | 1984年 / 19卷 / 5-6期
关键词：
D O I：
10.1016/0045-7949(84)90186-X
中图分类号：
TP39 [计算机的应用];
学科分类号：
081203 ; 0835 ;
摘要：
引用
收藏
页码：849 / 863
页数：15
相关论文
共 10 条
  • [1] ON MAKING THINGS THE BEST - AERONAUTICAL USES OF OPTIMIZATION
    ASHLEY, H
    [J]. JOURNAL OF AIRCRAFT, 1982, 19 (01): : 5 - 28
  • [2] COOK FE, 1956, NACA1278 REP
  • [3] FUNG FC, 1955, J APPL MECH, V22, P449
  • [4] MIURA H, 1971, 48 CAS W RES U DIV S
  • [5] STRUCTURAL OPTIMIZATION WITH FLUTTER SPEED CONSTRAINTS USING MAXIMIZED STEP SIZE
    OCONNELL, RF
    RADOVCICH, NA
    HASSIG, HJ
    [J]. JOURNAL OF AIRCRAFT, 1977, 14 (01): : 85 - 89
  • [6] ANALYTICAL AND EXPERIMENTAL STUDIES ON DYNAMIC LOADS IN AIRPLANE STRUCTURES DURING LANDING
    PIAN, THH
    FLOMENHOFT, HI
    [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (12): : 765 - &
  • [7] PIAN THH, 1950, J AERONAUT SCI, V17, P786
  • [8] Rao K.R, 2017, YOGA PSYCHOL THEORY
  • [9] RAO SS, 1982, SHOCK VIBRATION DIGE, V14, P9
  • [10] SCHMIT LA, 1965, NASA CR144
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