High Level Noise-Induced Bypass Transition in Compressible Plane Poiseuille Flow(Compressible Flow and Detonation)

    • YAHYAOUI Al Moez
    • Department of Mechanical Engineering and Intelligent Systems, The University of Electro-Communications
    • MAEKAWA Hiroshi
    • Department of Mechanical Engineering and Intelligent Systems, The University of Electro-Communications

Abstract

A numerical experiment is conducted to study the bypass transition of compressible plane Poiseuille flow. The space and time development of the disturbances into streaks is captured by employing a spatial DNS, which although requires more computational resources than the temporal one, allows having a full picture of the process. The generation and algebraic growth of the streaks, which are lifted away from the walls and oscillate in the spanwise direction, characterize the transition. The numerical results give some answers related to the transition of compressible plane channel flows, initiated by large amplitude random disturbances, and point to the universality of the breakdown mechanism in wall bounded flows (incompressible and subsonic) and to the important role of the near-wall streaks.

Journal

JSME international journal. Ser. B, Fluids and thermal engineering   [List of Volumes]

JSME international journal. Ser. B, Fluids and thermal engineering 45(2), 408-418, 2002-05-15  [Table of Contents]

The Japan Society of Mechanical Engineers

References:  20

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Codes

  • NII Article ID (NAID) :
    110003479054
  • NII NACSIS-CAT ID (NCID) :
    AA10888815
  • Text Lang :
    ENG
  • Article Type :
    ART
  • ISSN :
    13408054
  • NDL Article ID :
    6168284
  • NDL Source Classification :
    ZN11(科学技術--機械工学・工業)
  • NDL Call No. :
    Z53-Y271
  • Databases :
    CJP  NDL  NII-ELS  J-STAGE