Optimal wavepackets in streamwise corner flow

被引:5
|
作者
Schmidt, Oliver T. [1 ]
Hosseini, Seyed M. [2 ,3 ]
Rist, Ulrich [1 ]
Hanifi, Ardeshir [2 ,3 ,4 ]
Henningson, Dan S. [2 ,3 ]
机构
[1] Univ Stuttgart, Inst Aerodynam & Gasdynam, D-70569 Stuttgart, Germany
[2] KTH Mech, Linne Flow Ctr, SE-10044 Stockholm, Sweden
[3] KTH Mech, E Sci Res Ctr SeRC, SE-10044 Stockholm, Sweden
[4] FOI, Swedish Def Res Agcy, SE-16490 Stockholm, Sweden
基金
瑞典研究理事会;
关键词
absolute/convective instability; boundary layer stability; boundary layers; LAMINAR BOUNDARY-LAYER; OPTIMAL DISTURBANCES; LINEAR INSTABILITY; OPTIMAL EXCITATION; COMPRESSIBLE FLOW; VISCOUS-FLOW; STABILITY; PERTURBATIONS; TRANSITION;
D O I
10.1017/jfm.2015.18
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The global non-modal stability of the flow in a right-angled streamwise corner is investigated. Spatially confined linear optimal initial conditions and responses are obtained by use of direct-adjoint looping. Two base states are considered, the classical self-similar solution for a zero streamwise pressure gradient, and a modified solution that mimics leading-edge effects commonly observed in experimental studies. The latter solution is obtained in a reverse engineering fashion from published measurement data. Prior to the global analysis, a classical local linear stability and sensitivity analysis of both base states is conducted. It is found that the base-flow modification drastically reduces the critical Reynolds number through an inviscid mechanism, the so-called corner mode. A survey of the geometry of the two base states confirms that the modification greatly aggravates the inflectional nature of the flow. Global optimals are calculated for subcritical and supercritical Reynolds numbers, and for two finite optimization times. The optimal initial conditions are found to be self-confined in the spanwise directions, and symmetric with respect to the corner bisector. They evolve into streaks or streamwise modulated wavepackets, depending on the base state. Substantial transient growth caused by the Orr mechanism and the lift-up effect is observed.
引用
收藏
页码:405 / 435
页数:31
相关论文
共 50 条
  • [31] Numerical investigation of classical and bypass transition in streamwise corner-flow
    Schmidt, Oliver T.
    Rist, Ulrich
    IUTAM-ABCM SYMPOSIUM ON LAMINAR TURBULENT TRANSITION, 2015, 14 : 218 - 226
  • [32] VISCOUS SUBLAYER IN A STREAMWISE CORNER
    MOJOLA, OO
    JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1978, 45 (01): : 219 - 221
  • [33] Direct Numerical Simulation of Boundary Layer Transition in Streamwise Corner-Flow
    Schmidt, Oliver
    Selent, Bjoern
    Rist, Ulrich
    HIGH PERFORMANCE COMPUTING IN SCIENCE AND ENGINEERING'13: TRANSACTIONS OF THE HIGH PERFORMANCE COMPUTING CENTER, STUTTGART (HLRS) 2013, 2013, : 337 - 348
  • [34] Control and Entropy Analysis of Corner Flow Separation in a Compressor Cascade Using Streamwise Grooves
    Yi, Weilin
    Ji, Lucheng
    ENTROPY, 2019, 21 (10)
  • [35] Review of research on streamwise corner boundary layer
    Yang, Rui
    Wang, Qi
    Dong, Ze-Yu
    Zhao, Yu-Xin
    PHYSICS OF FLUIDS, 2023, 35 (08)
  • [36] Turbulent flows along a streamwise external corner
    Nikitin, Nikolay
    Krasnopolsky, Boris
    JOURNAL OF FLUID MECHANICS, 2022, 940
  • [37] EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER IN A STREAMWISE CORNER
    ZAMIR, M
    YOUNG, AD
    AERONAUTICAL QUARTERLY, 1970, 21 (NOV): : 313 - &
  • [39] The static pressure field as a driving mechanism for the streamwise corner flow in the presence of an inclined transverse plane
    Georgiou, Demos P.
    Milidonis, Kypros F.
    EXPERIMENTS IN FLUIDS, 2014, 55 (03)
  • [40] Space-time dynamics of optimal wavepackets for streaks in a channel entrance flow
    Alizard, F.
    Cadiou, A.
    Le Penven, L.
    Di Pierro, B.
    Buffat, M.
    JOURNAL OF FLUID MECHANICS, 2018, 844 : 669 - 706