Evaluation of Vortex Generators for Separation Control in a Transcritical Cylinder Flow

被引:7
|
作者
Shur, Michael L. [1 ,2 ]
Strelets, Michael K. [1 ,2 ,3 ]
Travin, Andrey K. [2 ]
Spalart, Philippe R. [4 ]
机构
[1] St Petersburg State Polytech Univ, Lab Computat Aeroacoust & Turbulence, St Petersburg 195220, Russia
[2] St Petersburg State Polytech Univ, New Technol & Serv, St Petersburg 195220, Russia
[3] St Petersburg State Polytech Univ, Lab Computat Aeroacoust & Turbulence, Lab, St Petersburg 195220, Russia
[4] Boeing Co, Boeing Commercial Airplanes, Flight Sci, Seattle, WA 98124 USA
关键词
CIRCULAR-CYLINDER; TURBULENCE MODELS; BOUNDARY-LAYER;
D O I
10.2514/1.J053851
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A numerical study is presented, aimed at evaluating the capability of vortex generators to produce a significant delay of separation and drag reduction in flows past smooth bluff bodies in the transcritical flow regime, with turbulent boundary layers ahead of separation. A fairly large series of steady Reynolds-averaged Navier-Stokes computations is carried out of the incompressible flow past a circular cylinder, with a simple and generic geometry, with and without vortex generators. Their effect is emulated with a body force, applied in a refined-grid region, instead of gridding the actual geometry. The flow is treated as steady, for reasons that are discussed. The parametric study includes 10 different vortex generator designs, as well as varying positions, spacings, and heights. Drag reductions of up to 60% are obtained, including those with sub-boundary-layer designs, with a height equal to half the boundary-layer thickness. Design recommendations are given, with the tolerance to vortex shedding and other variations in the flow conditions taken into account.
引用
收藏
页码:2967 / 2977
页数:11
相关论文
共 50 条
  • [1] Flow separation control and performance evaluation of an asymmetric diffuser using vortex generators
    Lu, Frank K.
    James, Sandeep E.
    Zhang, Liwei
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 136
  • [2] Use of vortex generators to control internal supersonic flow separation
    Szumowski, A
    Wojciechowski, J
    [J]. AIAA JOURNAL, 2005, 43 (01) : 216 - 218
  • [3] Control of Fin Shock Induced Flow Separation Using Vortex Generators
    Pickles, Joshua D.
    Narayanaswamy, Venkateswaran
    [J]. AIAA JOURNAL, 2020, 58 (11) : 4794 - 4806
  • [4] Application of micro-vortex generators for turbulent flow separation control
    Lin, JC
    [J]. IUTAM SYMPOSIUM ON MECHANICS OF PASSIVE AND ACTIVE FLOW CONTROL, 1999, 53 : 81 - 88
  • [5] SMALL SUBMERGED VORTEX GENERATORS FOR TURBULENT-FLOW SEPARATION CONTROL
    LIN, JC
    HOWARD, FG
    SELBY, GV
    [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1990, 27 (05) : 503 - 507
  • [6] Design and Scaling of Plasma Streamwise Vortex Generators for Flow Separation Control
    Kelley, Christopher L.
    Corke, Thomas C.
    Thomas, Flint O.
    Patel, Mehul
    Cain, Alan B.
    [J]. AIAA JOURNAL, 2016, 54 (11) : 3397 - 3408
  • [7] VISUALIZATION OF FLOW SEPARATION AND CONTROL BY VORTEX GENERATORS ON AN SINGLE FLAP IN LANDING CONFIGURATION
    Souckova, Natalie
    Kuklova, Jana
    Popelka, Lukas
    Matejka, Milan
    [J]. EXPERIMENTAL FLUID MECHANICS 2010, 2010, : 617 - 628
  • [8] VISUALIZATION OF FLOW SEPARATION AND CONTROL BY VORTEX GENERATORS ON AN SINGLE FLAP IN LANDING CONFIGURATION
    Souckova, Natalie
    Kuklova, Jana
    Popelka, Lukas
    Matejka, Milan
    [J]. EFM11 - EXPERIMENTAL FLUID MECHANICS 2011, 2012, 25
  • [9] Flow Separation Control on a Race Car Wing With Vortex Generators in Ground Effect
    Kuya, Yuichi
    Takeda, Kenji
    Zhang, Xin
    Beeton, Scott
    Pandaleon, Ted
    [J]. JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2009, 131 (12): : 1211021 - 1211028
  • [10] Optimized vortex generators in the flow separation control around a NACA 0015 profile
    Tebbiche, H.
    Boutoudj, M. S.
    [J]. EURODYN 2014: IX INTERNATIONAL CONFERENCE ON STRUCTURAL DYNAMICS, 2014, : 3219 - 3226