Active flow-separation control on a high-lift wing-body configuration

被引:0
|
作者
机构
[1] [1,Ciobaca, Vlad
[2] 1,Kühn, Timo
[3] 1,Rudnik, Ralf
[4] 2,Bauer, Matthias
[5] 3,Gölling, Burkhard
[6] 4,Breitenstein, Wiebke
来源
Ciobaca, V. | 1600年 / AIAA International卷 / 50期
关键词
43;
D O I
暂无
中图分类号
学科分类号
摘要
Journal article (JA)
引用
收藏
相关论文
共 50 条
  • [31] Active Flow Control of a High-Lift Supercritical Airfoil with Microjet Actuators
    Aley, Kade Stephen
    Guha, Tufan Kumar
    Kumar, Rajan
    AIAA JOURNAL, 2020, 58 (05) : 2053 - 2069
  • [32] Design of a high-lift experiment in water including active flow control
    Beutel, T.
    Sattler, S.
    El Sayed, Y.
    Schwerter, M.
    Zander, M.
    Buetgenbach, S.
    Leester-Schaedel, M.
    Radespiel, R.
    Sinapius, M.
    Wierach, P.
    SMART MATERIALS AND STRUCTURES, 2014, 23 (07)
  • [33] Control of Transonic Buffet by Shock Control Bumps on Wing-Body Configuration
    Mayer, R.
    Lutz, T.
    Kraemer, E.
    Dandois, J.
    JOURNAL OF AIRCRAFT, 2019, 56 (02): : 556 - 568
  • [34] Simulation of flow separation at the wing-body junction with different fairings
    Li, Chunna
    Ye, Zhengyin
    Wang, Gang
    JOURNAL OF AIRCRAFT, 2008, 45 (01): : 258 - 266
  • [35] Rear fuselage transonic flow characteristics for a complete wing-body configuration
    Coustols, E
    Seraudie, A
    Mignosi, A
    JOURNAL OF AIRCRAFT, 1997, 34 (03): : 337 - 345
  • [36] Investigation of micro vortex generators on controlling flow separation over SCCH high-lift configuration
    Chu HuBing
    Zhang BinQian
    Chen YingChun
    Li YaLin
    Mao Jun
    SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2012, 55 (07) : 1943 - 1953
  • [37] DEVELOPMENT OF ADVANCED CIRCULATION CONTROL WING HIGH-LIFT AIRFOILS
    ENGLAR, RJ
    HUSON, GG
    JOURNAL OF AIRCRAFT, 1984, 21 (07): : 476 - 483
  • [38] Investigation of micro vortex generators on controlling flow separation over SCCH high-lift configuration
    CHU HuBing ZHANG BinQian CHEN YingChun LI YaLin MAO Jun School of AeronauticsNorthwestern Polytechnical UniversityXian China Commercial Aircraft Corporation of China LtdShanghai Aircraft Design and Research InstituteShanghai China
    Science China(Technological Sciences), 2012, 55 (07) : 1943 - 1953
  • [39] ANALYSIS OF HIGH-LIFT WING SYSTEMS
    GORADIA, SH
    COLWELL, GT
    AERONAUTICAL QUARTERLY, 1975, 26 (MAY): : 88 - 108
  • [40] Mach number effects on buffeting flow on a half wing-body configuration
    Sartor, Fulvio
    Timme, Sebastian
    INTERNATIONAL JOURNAL OF NUMERICAL METHODS FOR HEAT & FLUID FLOW, 2016, 26 (07) : 2066 - 2080