3-DIMENSIONAL SOLUTION OF FLOWS OVER WINGS WITH LEADING-EDGE VORTEX SEPARATION

被引：8
|
作者：
WEBER, JA [1 ]
BRUNE, GW [1 ]
JOHNSON, FT [1 ]
LU, P [1 ]
RUBBERT, PE [1 ]
机构：
[1] BOEING CO,SEATTLE,WA 98124
来源：
AIAA JOURNAL | 1976年 / 14卷 / 04期
关键词：
D O I：
10.2514/3.61391
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：519 / 525
页数：7
相关论文
共 50 条
  • [1] 3-DIMENSIONAL FLOW OVER WINGS WITH LEADING-EDGE VORTEX SEPARATION
    JOHNSON, FT
    TINOCO, EN
    LU, P
    EPTON, MA
    AIAA JOURNAL, 1980, 18 (04) : 367 - 380
  • [2] 3-DIMENSIONAL VORTEX STRUCTURE IN A LEADING-EDGE SEPARATION BUBBLE AT MODERATE REYNOLDS-NUMBERS
    SASAKI, K
    KIYA, M
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 1991, 113 (03): : 405 - 410
  • [3] Leading-edge vortex stability in insect wings
    Minotti, FO
    Speranza, E
    PHYSICAL REVIEW E, 2005, 71 (05):
  • [4] FUNDAMENTAL AERODYNAMIC CHARACTERISTICS OF DELTA-WINGS WITH LEADING-EDGE VORTEX FLOWS
    WOOD, RM
    MILLER, DS
    JOURNAL OF AIRCRAFT, 1985, 22 (06): : 479 - 485
  • [5] OSCILLATING SLENDER WINGS WITH LEADING-EDGE SEPARATION
    RANDALL, DG
    AERONAUTICAL QUARTERLY, 1966, 17 : 311 - &
  • [6] Leading-edge vortex dynamics on plunging airfoils and wings
    Son, O.
    Gao, A-K
    Gursul, I
    Cantwell, C. D.
    Wang, Z.
    Sherwin, S. J.
    JOURNAL OF FLUID MECHANICS, 2022, 940
  • [7] Leading-edge vortex shedding from rotating wings
    Kolomenskiy, Dmitry
    Elimelech, Yossef
    Schneider, Kai
    FLUID DYNAMICS RESEARCH, 2014, 46 (03)
  • [8] VORTEX SHEET SHORTENING IN THE SMITH MODEL FOR SLENDER DELTA WINGS WITH LEADING-EDGE SEPARATION
    LAMMLEIN, S
    WAGNER, B
    ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1983, 7 (04): : 279 - 281
  • [9] SLENDER WINGS WITH LEADING-EDGE VORTEX SEPARATION - A CHALLENGE FOR PANEL METHODS AND EULER SOLVERS
    HITZEL, SM
    SCHMIDT, W
    JOURNAL OF AIRCRAFT, 1984, 21 (10): : 751 - 759
  • [10] AERODYNAMICS OF MANEUVERING SLENDER WINGS WITH LEADING-EDGE SEPARATION
    TAVARES, TS
    MCCUNE, JE
    AIAA JOURNAL, 1993, 31 (06) : 977 - 986
12345