DELTA WING SHOCK SHAPE AT HYPERSONIC SPEED

被引：2
|
作者：
RAO, DM
机构：
来源：
AIAA JOURNAL | 1971年 / 9卷 / 10期
关键词：
D O I：
10.2514/3.6479
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：2093 / &
相关论文
共 50 条
  • [1] HYPERSONIC FLOW PAST A DELTA WING
    GONOR, AL
    JOURNAL OF APPLIED MATHEMATICS AND MECHANICS-USSR, 1970, 34 (03): : 452 - &
  • [2] Mass Transfer on a Delta Wing in a Hypersonic Flow
    G. N. Dudin
    Fluid Dynamics, 2002, 37 : 328 - 335
  • [3] DELTA WING IN HYPERSONIC GAS-FLOW
    GOLUBINSKII, AI
    GOLUBKIN, VN
    DOKLADY AKADEMII NAUK SSSR, 1976, 226 (04): : 789 - 790
  • [4] Mass Transfer on a Delta Wing in a Hypersonic Flow
    Dudin, G. N.
    FLUID DYNAMICS, 2002, 37 (02) : 328 - 335
  • [5] INVESTIGATION OF LEEWARD SIDE OF A DELTA WING AT HYPERSONIC SPEEDS
    CROSS, EJ
    HANKEY, WL
    JOURNAL OF SPACECRAFT AND ROCKETS, 1969, 6 (02) : 185 - &
  • [6] Optimization of the shape of a wing in a hypersonic nonequilibrium gas flow
    Golubkin V.N.
    Postnov D.S.
    Fluid Dynamics, 2000, 35 (2) : 288 - 296
  • [7] Shape Optimization for Hypersonic Arc-Wing Missiles
    Cui, Kai
    Yang, Guo-wei
    JOURNAL OF SPACECRAFT AND ROCKETS, 2010, 47 (04) : 694 - 700
  • [8] A SIMILARITY LAW FOR THE NORMAL FORCE ON A DELTA WING AT HYPERSONIC SPEEDS
    MESSITER, AF
    JOURNAL OF THE AEROSPACE SCIENCES, 1959, 26 (02): : 119 - 120
  • [9] HYPERSONIC FLOW PAST A DELTA WING AT LARGE ANGLES OF ATTACK
    GOLUBKIN, VN
    PMM JOURNAL OF APPLIED MATHEMATICS AND MECHANICS, 1984, 48 (03): : 270 - 275
  • [10] Instability and Transition of Hypersonic Boundary Layer on a Blunted Delta Wing
    Yao, Shiyong
    Duan, Yi
    Tian, Chuan
    Li, Siyi
    Yang, Pan
    Duan, Hui Shen
    JOURNAL OF SPACECRAFT AND ROCKETS, 2023, 60 (01) : 38 - 48
12345