Reynolds number scaling effects on the european high-lift project configurations

被引：0
|
作者：
Rudnik, R. [1 ,3 ]
Germain, E. [2 ,4 ]
机构：
[1] DLR, German Aerospace Center, 38108 Brunswick, Germany
[2] European Transonic Wind Tunnel, D-51147 Cologne, Germany
[3] Institute of Aerodynamics and Flow Technology, Lilienthalplatz 7, DEU
[4] Ernst-Mach Strasse
来源：
Journal of Aircraft | 2009年 / 46卷 / 04期
关键词：
10;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Journal article (JA)
引用
收藏
页码：1140 / 1151
相关论文
共 50 条
  • [21] COMPUTATIONAL ANALYSIS OF A HIGH-LIFT AND LOW REYNOLDS NUMBER AIRFOIL AT TURBULENT ATMOSPHERIC CONDITIONS
    Islam, Mazharul
    Amin, M. Ruhul
    Shariff, Yasir M.
    IMECE 2009: PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, VOL 9, PTS A-C, 2010, : 867 - 874
  • [22] Parametric investigation of a high-lift airfoil at high Reynolds numbers
    Lin, JC
    Dominik, CJ
    JOURNAL OF AIRCRAFT, 1997, 34 (04): : 485 - 491
  • [23] Parametric investigation of a high-lift airfoil at high Reynolds numbers
    NASA Langley Research Cent, Hampton, United States
    J Aircr, 4 (485-491):
  • [24] Numerical Simulation of Low-Reynolds-Number and High-Lift Airfoil S1223
    Ma, Rong
    Liu, Peiqing
    WORLD CONGRESS ON ENGINEERING 2009, VOLS I AND II, 2009, : 1691 - +
  • [25] THE INFLUENCE OF MACH NUMBER ON THE BOUNDARY LAYER DEVELOPMENT OF HIGH-LIFT LOW PRESSURE TURBINE IN LOW REYNOLDS NUMBER
    Duan, Wenhua
    Liu, Jian
    Qiao, Weiyang
    PROCEEDINGS OF THE ASME TURBO EXPO 2020: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 2E, PT I, 2020,
  • [26] Numerical investigation on the aerodynamics of high-lift and bird-like low Reynolds number airfoils
    Boughou, Smail
    Omar, Ashraf A.
    Elsayed, Omer A.
    Aldheeb, Mohammed
    PROGRESS IN COMPUTATIONAL FLUID DYNAMICS, 2023, 23 (03): : 146 - 162
  • [27] Numerical analysis of high-lift configurations with oscillating flaps
    Ruhland J.
    Breitsamter C.
    CEAS Aeronautical Journal, 2021, 12 (02) : 345 - 359
  • [28] A study on the mechanism of high-lift generation by an insect wing in unsteady motion at small Reynolds number
    Hamdani, Hossein Raza
    Naqvi, Ali
    INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2011, 67 (05) : 581 - 598
  • [29] Reynolds number and wind tunnel wall effects on the flow field around a generic UHBR engine high-lift configuration
    Ullah J.
    Prachař A.
    Šmíd M.
    Seifert A.
    Soudakov V.
    Lutz T.
    Krämer E.
    CEAS Aeronautical Journal, 2020, 11 (04) : 1009 - 1023
  • [30] Grid generation about high-lift wing configurations
    Adhikari, Nirajan
    Stephen Nichols, D.
    Numerical Simulation of the Aerodynamics of High-Lift Configurations, 2018, : 9 - 26
12345