VORTEX SHEET SHORTENING IN THE SMITH MODEL FOR SLENDER DELTA WINGS WITH LEADING-EDGE SEPARATION

被引：0
|
作者：
LAMMLEIN, S [1 ]
WAGNER, B [1 ]
机构：
[1] DORNIER GMBH,THEORET AERODYNAM ABT,D-7990 FRIEDRICHSHAFEN 1,FED REP GER
来源：
ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG | 1983年 / 7卷 / 04期
关键词：
D O I：
暂无
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：279 / 281
页数：3
相关论文
共 50 条
  • [21] Leading-edge vortex structure of nonslender delta wings at low Reynolds number
    Ol, MV
    Gharib, M
    AIAA JOURNAL, 2003, 41 (01) : 16 - 26
  • [22] CONNECTION BETWEEN LEADING-EDGE SWEEP, VORTEX LIFT, AND VORTEX STRENGTH FOR DELTA-WINGS
    HEMSCH, MJ
    LUCKRING, JM
    JOURNAL OF AIRCRAFT, 1990, 27 (05): : 473 - 475
  • [23] 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
  • [24] Leading-edge vortex dynamics on a slender oscillating wing
    Jun, Young-Whoon
    Nelson, Robert C.
    1600, (25):
  • [25] EFFECTS OF LEADING-EDGE CAMBER ON LOW-SPEED CHARACTERISTICS OF SLENDER DELTA WINGS.
    Wentz, W.H.
    Wichita State Univ, Kans
    NASA Contractor Reports, 1972,
  • [26] LEADING-EDGE VORTEX DYNAMICS ON A SLENDER OSCILLATING WING
    JUN, YW
    NELSON, RC
    JOURNAL OF AIRCRAFT, 1988, 25 (09): : 815 - 819
  • [27] 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
  • [28] NONUNIFORM MOTION OF LEADING-EDGE VORTEX BREAKDOWN ON RAMP PITCHING DELTA-WINGS
    MIAU, JJ
    CHANG, RC
    CHOU, JH
    LIN, CK
    AIAA JOURNAL, 1992, 30 (07) : 1691 - 1702
  • [29] Leading-edge vortex shedding from rotating wings
    Kolomenskiy, Dmitry
    Elimelech, Yossef
    Schneider, Kai
    FLUID DYNAMICS RESEARCH, 2014, 46 (03)
  • [30] LIFT OF DELTA-WINGS WITH LEADING-EDGE BLOWING
    TAVELLA, DA
    JOURNAL OF AIRCRAFT, 1988, 25 (06): : 522 - 524
12345