ジェット吹出しによる境界層能動制御のメカニズム  [in Japanese] The Mechanism of Active Boundary Layer Control Using Vortex Generator Jets  [in Japanese]

Abstract

The vortex generator jet method is active control of flow separation that has the ability to provide a time-varying control action. The mechanism for suppressing flow separation was studied experimentally by making a comparison between two effects of steady and pulsed jets on generating longitudinal vortices. The suppression of flow separation is accomplished by transporting high momentum fluid of the freestream to the lower wall by the secondary flow of longitudinal vortices. However, if the vortex detaches from the wall, a counter-rotating vortex of nearly equal strength is induced and, thus, an upwash region is produced by the effect of a vortex pair. The upwash makes ineffective the secondary flow toward the lower wall and as a result streamwise velocity decreases. Pulsed jets enhance the mixing process in comparison with steady jets and indicate effective separation control for the purpose of attaching the vortex to the lower wall.

Journal

Transactions of the Japan Society of Mechanical Engineers. B   [List of Volumes]

Transactions of the Japan Society of Mechanical Engineers. B 64(617), 92-99, 1998-01-25  [Table of Contents]

The Japan Society of Mechanical Engineers

References:  5

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Cited by:  9

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Codes

  • NII Article ID (NAID) :
    110002396762
  • NII NACSIS-CAT ID (NCID) :
    AN00187441
  • Text Lang :
    JPN
  • Article Type :
    Journal Article
  • ISSN :
    03875016
  • NDL Article ID :
    4391004
  • NDL Source Classification :
    ZN11(科学技術--機械工学・工業)
  • NDL Call No. :
    Z16-109
  • Databases :
    CJP  CJPref  NDL  NII-ELS