AERODYNAMICS OF HIGH LIFT ILLUSTRATED BY AUGMENTOR-WING RESEARCH

被引：0
|
作者：
WHITTLEY, DC
机构：
来源：
CANADIAN AERONAUTICS AND SPACE JOURNAL | 1972年 / 18卷 / 02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：33 / &
相关论文
共 50 条
  • [31] Grid generation about high-lift wing configurations
    Adhikari, Nirajan
    Stephen Nichols, D.
    Numerical Simulation of the Aerodynamics of High-Lift Configurations, 2018, : 9 - 26
  • [32] Aerodynamics of a Common Research Model Wing with Leading-Edge Ice Shape
    Stebbins, Spencer
    Loth, Eric
    Broeren, Andy
    Potapczuk, Mark
    Porter, Christopher
    JOURNAL OF AIRCRAFT, 2021, 58 (04): : 894 - 906
  • [33] Numerical simulation technology of high lift trapezoidal wing configuration
    Wang, Yuntao, 1600, Chinese Society of Astronautics (35):
  • [34] Transition measurement and analysis on a swept wing in high lift configuration
    Séraudie, A
    Perraud, J
    Moens, F
    AEROSPACE SCIENCE AND TECHNOLOGY, 2003, 7 (08) : 569 - 576
  • [35] Hysteresis and broad flow features on a swept wing at high lift
    Venkatakrishnan, L.
    Sundaram, S.
    Viswanath, P. R.
    JOURNAL OF AIRCRAFT, 2006, 43 (04): : 1036 - 1043
  • [36] Concurrent wing and high-lift system aerostructural optimization
    Koen T. H. van den Kieboom
    Ali Elham
    Structural and Multidisciplinary Optimization, 2018, 57 : 947 - 963
  • [37] Propeller and Active High Lift Wing Interaction in Experiment and Simulation
    Lenfers, Carsten
    Beck, Nils
    Bauer, Marc
    NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS X, 2016, 132 : 51 - 61
  • [38] HIGH-LIFT WING SECTION FOR LIGHT AIRCRAFT.
    Marsden, D.J.
    Canadian Aeronautics and Space Journal, 1988, 34 (01): : 55 - 61
  • [39] Modeling the turbulent vortex wake of high-lift wing
    Spalart, F.P.
    Strelets, M.Kh.
    Travin, A.K.
    Shur, M.L.
    Izvestiya Akademii Nauk. Mekhanika Zhidkosti I Gaza, 2001, (05): : 64 - 73
  • [40] Numerical simulations of streamwise vortices on a high-lift wing
    Landa T.
    Radespiel R.
    Wild J.
    CEAS Aeronautical Journal, 2017, 8 (1) : 3 - 15
12345