EFFECTS OF DISCONTINUOUS DROOPED WING LEADING-EDGE MODIFICATIONS ON THE SPINNING CHARACTERISTICS OF A LOW-WING GENERAL AVIATION AIRPLANE.

被引：0
|
作者：
DiCarlo, D.J.
Stough III, H.P.
Patton Jr., J.M.
机构：
来源：
AIAA Paper | 1980年
关键词：
Compendex;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Aircraft
引用
收藏
相关论文
共 42 条
  • [1] EFFECTS OF WING LEADING-EDGE DESIGN ON THE SPIN CHARACTERISTICS OF A GENERAL-AVIATION AIRPLANE
    DICARLO, DJ
    STOUGH, HP
    PATTON, JM
    JOURNAL OF AIRCRAFT, 1981, 18 (09): : 786 - 792
  • [2] EXPLORATORY STUDY OF THE EFFECTS OF WING-LEADING-EDGE MODIFICATIONS ON THE STALL/SPIN BEHAVIOR OF A LIGHT GENERAL AVIATION AIRPLANE.
    Anon
    NASA Technical Paper, 1979, (1589):
  • [3] DISCONTINUOUS WING LEADING-EDGE TO ENHANCE SPIN RESISTANCE
    DICARLO, DJ
    GLOVER, KE
    STEWART, EC
    STOUGH, HP
    JOURNAL OF AIRCRAFT, 1985, 22 (04): : 283 - 288
  • [4] Analysis of general-aviation aircraft wing sections with drooped leading edges
    Syms, G. F.
    JOURNAL OF AIRCRAFT, 2006, 43 (04): : 1029 - 1035
  • [5] Aerodynamic characteristics of morphing wing withflexible leading-edge
    Zi KAN
    Daochun LI
    Tong SHEN
    Jinwu XIANG
    Lu ZHANG
    Chinese Journal of Aeronautics , 2020, (10) : 2610 - 2619
  • [6] Aerodynamic characteristics of morphing wing with flexible leading-edge
    Kan, Zi
    Li, Daochun
    Shen, Tong
    Xiang, Jinwu
    Zhang, Lu
    CHINESE JOURNAL OF AERONAUTICS, 2020, 33 (10) : 2610 - 2619
  • [7] THERMODYNAMIC PERFORMANCE OF AN AIRPLANE WING LEADING-EDGE ANTI-ICING SYSTEM
    ROSS, R
    JOURNAL OF AIRCRAFT, 1984, 21 (07): : 536 - 537
  • [8] Effects of leading-edge tubercles on wing flutter speeds
    Ng, B. F.
    New, T. H.
    Palacios, R.
    BIOINSPIRATION & BIOMIMETICS, 2016, 11 (03)
  • [9] Flow structure modifications by leading-edge tubercles on a 3D wing
    Kim, Heesu
    Kim, Jooha
    Choi, Haecheon
    BIOINSPIRATION & BIOMIMETICS, 2018, 13 (06)
  • [10] Effects of leading-edge lateral blowing on delta wing aerodynamics
    Hong, JS
    Celik, ZZ
    Roberts, L
    AIAA JOURNAL, 1996, 34 (12) : 2471 - 2478
12345