Receptivity of the rotating disk boundary layer to traveling disturbances

被引:1
|
作者
Thomas, Christian [1 ]
机构
[1] Macquarie Univ, Sch Math & Phys Sci, Macquarie Pk, NSW 2109, Australia
关键词
TOLLMIEN-SCHLICHTING WAVES; SECONDARY INSTABILITY; ABSOLUTE INSTABILITY; NONSTATIONARY MODES; STEADY SUCTION; STABILITY; TRANSITION; FLOW; VORTICES; LAMINAR;
D O I
10.1063/5.0180608
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
An adjoint approach is developed to undertake a receptivity study of the rotating disk boundary layer. The adjoint linearized Navier-Stokes equations are first derived in cylindrical coordinates. A receptivity formula is then formulated that specifies the response of stationary and traveling linear perturbations to an external force, including sources of momenta and mass and unsteady wall motion. Using the parallel flow approximation, in which the radial dependence of the undisturbed flow is ignored, receptivity characteristics are computed for a broad range of temporal frequencies, radial wavenumbers, azimuthal mode numbers, and Reynolds numbers. The type-I crossflow instability attains a maximum amplitude for external forces fixed near the wall-normal location of the critical layer (i.e., alpha F-r + beta G = omega), and the type-II Coriolis instability achieves larger amplitudes when external forces are located in the vicinity of a vanishing effective shear stress (i.e., alpha F-r ' + beta G' = 0). Sources of radial momenta fixed about these wall-normal locations establish larger-sized disturbances than equivalent-sized sources of azimuthal momenta, wall-normal momenta, and mass. At the disk surface, motion along the wall-normal direction induces a stronger receptivity response than wall motions acting along the radial and azimuthal directions. In general, the crossflow instability achieves larger-sized amplitudes than the Coriolis instability, with the peak response realized for Reynolds numbers near the critical conditions for linear instability. (c) 2024 Author(s). All article content, except where otherwise noted, is licensed under a Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/)
引用
下载
收藏
页数:16
相关论文
共 50 条
  • [1] Boundary-layer receptivity to freestream disturbances
    Saric, WS
    Reed, HL
    Kerschen, EJ
    ANNUAL REVIEW OF FLUID MECHANICS, 2002, 34 : 291 - 319
  • [2] Receptivity of hypersonic boundary layer to wall disturbances
    Fedorov, AV
    Khokhlov, AP
    THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS, 2002, 15 (04) : 231 - 254
  • [3] Receptivity of Hypersonic Boundary Layer to Wall Disturbances
    A.V. Fedorov
    A.P. Khokhlov
    Theoretical and Computational Fluid Dynamics, 2002, 15 : 231 - 254
  • [4] Receptivity of a Supersonic Boundary Layer to Acoustic Disturbances
    Balakumar, P.
    AIAA JOURNAL, 2009, 47 (05) : 1069 - 1078
  • [5] Boundary-layer receptivity to transient convected disturbances
    Dietz, AJ
    AIAA JOURNAL, 1998, 36 (07) : 1171 - 1177
  • [6] BOUNDARY-LAYER RECEPTIVITY TO ACOUSTIC DISTURBANCES.
    Zhigulev, V.N.
    Fedorov, A.V.
    Journal of applied mechanics and technical physics, 1987, 28 (01) : 28 - 34
  • [7] BOUNDARY LAYER MEASUREMENTS ON A ROTATING DISK
    Raghav, Vrishank
    Komerath, Narayanan
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2013, VOL 7B, 2014,
  • [8] Numerical simulation of receptivity of a hypersonic boundary layer to acoustic disturbances
    Maslov, A. A.
    Kudryavtsev, A. N.
    Mironov, S. G.
    Poplavskaya, T. V.
    Tsyryulnikov, I. S.
    JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS, 2007, 48 (03) : 368 - 374
  • [9] Numerical modeling of the receptivity of a supersonic boundary layer to acoustic disturbances
    I. V. Egorov
    V. G. Sudakov
    A. V. Fedorov
    Fluid Dynamics, 2006, 41
  • [10] Numerical modeling of the receptivity of a supersonic boundary layer to entropy disturbances
    A. A. Ryzhov
    V. G. Sudakov
    Fluid Dynamics, 2012, 47 : 338 - 345