Modeling the turbulent vortex wake of high-lift wing

被引：0
|
作者：
Spalart, F.P.
Strelets, M.Kh.
Travin, A.K.
Shur, M.L.
机构：
来源：
Izvestiya Akademii Nauk. Mekhanika Zhidkosti I Gaza | 2001年 / 05期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：64 / 73
相关论文
共 50 条
  • [31] Platform for Transport Aircraft Wing-Body Parametric Modeling and High-Lift System Design
    Tian, Yun
    Qu, Xiangnan
    Liu, Peiqing
    Yan, Shiwei
    JOURNAL OF AEROSPACE ENGINEERING, 2017, 30 (05)
  • [32] Transition on a high-lift swept wing in the European project EUROLIFT
    Perraud, J
    Séraudie, A
    Moens, F
    JOURNAL OF AIRCRAFT, 2004, 41 (05): : 1183 - 1190
  • [33] Prediction of high-lift flows using turbulent closure models
    Rumsey, CL
    Gatski, TB
    Ying, SX
    Bertelrud, A
    AIAA JOURNAL, 1998, 36 (05) : 765 - 774
  • [34] Experimental investigations on steady wake effects in a high-lift turbine cascade
    Wolfram Heinke
    Sven König
    Berthold Matyschok
    Bernd Stoffel
    Andreas Fiala
    Klaus Heinig
    Experiments in Fluids, 2004, 37 : 488 - 496
  • [35] Experimental investigations on steady wake effects in a high-lift turbine cascade
    Heinke, W
    König, S
    Matyschok, B
    Stoffel, B
    Fiala, A
    Heinig, K
    EXPERIMENTS IN FLUIDS, 2004, 37 (04) : 488 - 496
  • [36] Investigation on application of high-lift configuration to wing-in-ground effect
    Yang, W.
    Lin, F.
    Yang, Z.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2012, 226 (G3) : 260 - 271
  • [37] Investigations on the influence of fins on the extended nearfield of a wing in high-lift configuration
    Kauertz, Sebastian
    Neuwerth, Guenther
    Schoell, Robert
    NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS V, 2006, 92 : 33 - +
  • [38] Aerodynamics of the Wing/Fuselage Junction at an Transport Aircraft in High-Lift Configuration
    Melber-Wilkending, Stefan
    NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS VII, 2010, 112 : 529 - 536
  • [39] High-lift design for a forward swept natural laminar flow wing
    Keller D.
    CEAS Aeronautical Journal, 2020, 11 (1) : 81 - 92
  • [40] Nested collaborative optimization of laminar wing and its high-lift devices
    Luo J.
    Song W.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2022, 43 (08):
12345