EFFECTS OF VORTEX FLAPS ON THE LOW-SPEED AERODYNAMIC CHARACTERISTICS OF AN ARROW WING.

被引：0
|
作者：
Yip, Long P.
Murri, Daniel G.
机构：
来源：
NASA Technical Paper | 1981年
关键词：
ARROW WING;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
A low-speed wind-tunnel investigation was made to determine the longitudinal and lateral-directional aerodynamic effects of plain and tabbed vortex flaps on a flatplate, highly swept arrow-wind model. Flow-visualization studies were made using a helium-bubble technique. Static forces and moments were measured over an angle-of-attack range from 0 degree to 50 degree for sideslip angles of 0 degree and plus or minus 4 degree .
引用
收藏
相关论文
共 50 条
  • [1] LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A HIGHLY SWEPT, UNTWISTED, UNCAMBERED ARROW WING.
    Coe Jr., Paul L.
    Kjelgaard, Scott O.
    Gentry Jr., Garl L.
    NASA Technical Paper, 1983,
  • [2] FLAP EFFECTIVENESS ON SUBSONIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A MODIFIED ARROW WING.
    Quinto, P.Frank
    Paulson Jr., John W.
    NASA Technical Memorandum, 1983,
  • [3] Investigation of aerodynamic characteristics on an oscillating delta wing in low-speed
    Hong, Jinsen
    Fu, Guangming
    Wang, Qiang
    Qidong Shiyan yu Celiang Kongzhi/Aerodynamic Experiment and Measurement & Control, 12 (01): : 38 - 43
  • [4] COMPUTATIONAL AERODYNAMIC OPTIMIZATION OF A LOW-SPEED WING
    Lahuta, Martin
    Patek, Zdenek
    Szollos, Andras
    ACTA POLYTECHNICA, 2014, 54 (06) : 420 - 425
  • [5] VORTEX BREAKDWON EFFECTS ON LOW-SPEED AERODYNAMIC CHARACTERISTICS OF SLENDER DELTA WINGS IN SYMMETRICAL FLOW
    HUMMEL, D
    SRINIVAS.PS
    JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY, 1967, 71 (676): : 319 - &
  • [6] AERODYNAMIC CHARACTERISTICS OF STRAKE VORTEX FLAPS ON A STRAKE-WING CONFIGURATION
    TRAUB, LW
    VANDERMERWE, J
    JOURNAL OF AIRCRAFT, 1994, 31 (05): : 1116 - 1120
  • [7] PILOTED-SIMULATION STUDY OF EFFECTS OF VORTEX FLAPS ON LOW-SPEED HANDLING QUALITIES OF A DELTA-WING AIRPLANE.
    Brandon, Jay M.
    Brown, Philip W.
    Wunschel, Alfred J.
    NASA Technical Paper, 1987,
  • [8] Low-speed characteristics for the wing-canard configuration of the international vortex flow experiment
    Hummel, D.
    Oelker, H.-Chr.
    Journal of Aircraft, 1994, 31 (04): : 868 - 878
  • [9] LOW-SPEED CHARACTERISTICS FOR THE WING-CANARD CONFIGURATION OF THE INTERNATIONAL VORTEX FLOW EXPERIMENT
    HUMMEL, D
    OELKER, HC
    JOURNAL OF AIRCRAFT, 1994, 31 (04): : 868 - 878
  • [10] Low-speed aerodynamic characteristics improvement of ATR 42 airfoil using a morphing wing approach
    Gabor, Oliviu Sugar
    Koreanschi, Andreea
    Botez, Ruxandra Mihaela
    38TH ANNUAL CONFERENCE ON IEEE INDUSTRIAL ELECTRONICS SOCIETY (IECON 2012), 2012, : 5451 - 5456
12345