VISUALIZATION OF ACCELERATING FLOW AROUND AN AIRFOIL AT HIGH ANGLES OF ATTACK

被引：0
|
作者：
FREYMUTH, P
BANK, W
PALMER, M
机构：
来源：
ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG | 1983年 / 7卷 / 06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：392 / 400
页数：9
相关论文
共 50 条
  • [1] Unsteady Flow Around Airfoil at Large Angles of Attack
    Udartsev, E. P.
    Shvets, O. V.
    Pereverzev, O. M.
    Alekseenko, S. I.
    [J]. 2013 IEEE 2ND INTERNATIONAL CONFERENCE ON ACTUAL PROBLEMS OF UNMANNED AIR VEHICLES DEVELOPMENTS (APUAVD), 2013, : 65 - 67
  • [2] Unsteady characteristics of flow around an airfoil at high angles of attack and low Reynolds numbers
    Guo, Hui
    Yang, Hongxing
    Zhou, Yu
    Wood, David
    [J]. WIND ENERGY, 2007, : 211 - +
  • [3] TURBULENT FLOW CONTROL WITH VORTEX GENERATORS AROUND A SYMMETRICAL AIRFOIL AT HIGH ATTACK ANGLES
    Tebbiche, H.
    Boutoudj, M. S.
    [J]. JOURNAL OF THE SERBIAN SOCIETY FOR COMPUTATIONAL MECHANICS, 2019, 13 (02) : 67 - 86
  • [4] Simulation of flow around a slender body at high angles of attack
    Obeid, Osama
    Alqadi, Ibraheem
    [J]. 2017 2ND INTERNATIONAL CONFERENCE ON MECHANICAL, MANUFACTURING, MODELING AND MECHATRONICS (IC4M 2017) - 2017 2ND INTERNATIONAL CONFERENCE ON DESIGN, ENGINEERING AND SCIENCE (ICDES 2017), 2017, 104
  • [5] A Zonal RANS/LES Method for the Flow Around an Airfoil at High Angle of Attack
    Geurts, K. J.
    Meinke, M.
    Schroeder, W.
    [J]. NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS VIII, 2013, 121 : 465 - 472
  • [6] AIRFOIL COMPUTATION AT HIGH ANGLES OF ATTACK, INVISCID AND VISCOUS PHENOMENA
    BARTON, JT
    PULLIAM, TH
    [J]. AIAA JOURNAL, 1986, 24 (05) : 705 - 712
  • [7] Moving surface separation control for airfoil at high angles of attack
    Sengupta, T
    Gupta, VK
    Gopalan, G
    [J]. IUTAM SYMPOSIUM ON MECHANICS OF PASSIVE AND ACTIVE FLOW CONTROL, 1999, 53 : 243 - 248
  • [8] INVISCID HYPERSONIC FLOW AROUND A CONE AT ANGLES OF ATTACK
    CHANG, PK
    SMITH, RA
    OH, SK
    [J]. ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1972, 20 (04): : 141 - &
  • [9] The structure of turbulent flow behind the NACA 0012 airfoil at high angles of attack and low Reynolds number
    Yanovych, Vitalii
    Duda, Daniel
    Uruba, Vaclav
    Kosiak, Pavlo
    [J]. 20TH CONFERENCE ON POWER SYSTEM ENGINEERING, 2021, 345
  • [10] Investigations of Flow Phenomena Over a Flat Plate and NACA0012 Airfoil at High Angles of Attack
    Jha, Shailesh Kr
    Gautam, Uddipta
    Pawar, Pramod
    Narayanan, S.
    Kumaraswamidhas, L. A.
    [J]. IRANIAN JOURNAL OF SCIENCE AND TECHNOLOGY-TRANSACTIONS OF MECHANICAL ENGINEERING, 2020, 44 (04) : 985 - 996
12345