LIFT-CURVE SLOPE FOR FINITE-ASPECT-RATIO WINGS

被引:4
|
作者
LAITONE, EV
机构
来源
JOURNAL OF AIRCRAFT | 1989年 / 26卷 / 08期
关键词
D O I
10.2514/3.45841
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:789 / 790
页数:2
相关论文
共 50 条
  • [41] Three-dimensional indicial response of finite aspect ratio yawed wings
    Manglano-Villamarin, C. E.
    Shaw, S. T.
    AERONAUTICAL JOURNAL, 2007, 111 (1120): : 359 - 371
  • [42] Aspect ratio studies on insect wings
    Bhat, S. S.
    Zhao, J.
    Sheridan, J.
    Hourigan, K.
    Thompson, M. C.
    PHYSICS OF FLUIDS, 2019, 31 (12)
  • [43] On the mechanism of high-incidence lift generation for steadily translating low-aspect-ratio wings
    DeVoria, Adam C.
    Mohseni, Kamran
    JOURNAL OF FLUID MECHANICS, 2017, 813 : 110 - 126
  • [44] Disappearance of Vortex Lift in Low-Aspect-Ratio Wings at Very-low Reynolds Numbers
    Okamoto, Masato
    Sasaki, Daisuke
    Kamikubo, Masaya
    Fujii, Ryota
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2019, 62 (06) : 310 - 317
  • [45] Leading-Edge Vortex as a High-Lift Mechanism for Large-Aspect-Ratio Wings
    Ben-Gida, Hadar
    Gurka, Roi
    Weihs, Daniel
    AIAA JOURNAL, 2020, 58 (07) : 2806 - 2819
  • [46] Experimental Investigation of Vortex-Tube Streamwise-Vorticity Characteristics and Interaction Effects with a Finite-Aspect-Ratio Wing
    Carlson, Bailey
    Ullah, Al Habib
    Estevadeordal, Jordi
    FLUIDS, 2020, 5 (03)
  • [47] THE EFFECT OF THE BOUNDARY LAYER ON THE LIFT OF FINITE WINGS
    SQUIRE, LC
    AERONAUTICAL QUARTERLY, 1963, 14 (03): : 241 - 253
  • [48] WINGLETS ON LOW-ASPECT-RATIO WINGS
    KUHLMAN, JM
    LIAW, P
    JOURNAL OF AIRCRAFT, 1988, 25 (10): : 932 - 941
  • [49] Leading Edge Vortex Circulation Development on Finite Aspect Ratio Pitch-Up Wings
    Hord, Kyle
    Lian, Yongsheng
    AIAA JOURNAL, 2016, 54 (09) : 2755 - 2767
  • [50] Studies of the screening surface proximity on integral aerodynamic characteristics of rectangular high-lift wings of different aspect ratio
    Bukanov K.V.
    Zherekhov V.V.
    Russian Aeronautics (Iz VUZ), 2016, 59 (1) : 36 - 43