• DocumentCode
    3230829
  • Title

    New concepts about 4 hole wall stress probe

  • Author

    De Ponte, S. ; Gasparini, L. ; Gibertini, G. ; Codazzi, L.

  • Author_Institution
    Dipt. di Ingegneria Aerosp., Politecnico di Milano, Italy
  • fYear
    1997
  • fDate
    29 Sep-2 Oct 1997
  • Firstpage
    223
  • Lastpage
    227
  • Abstract
    For improving the wall shear stress measurement in a fluid stream, a new procedure for calibration of the “triangular probe” is developed. This new procedure allows to have thinner probes, completely submerged into the viscous sublayer, thus it is less intrusive and reduces the experimental perturbations. Comparisons to numerical results on an airfoil surface confirm the validity of this new procedure
  • Keywords
    aerospace test facilities; calibration; flow measurement; probes; stress measurement; wakes; aerospace testing; airfoil surface; calibration; fluid stream; numerical results; thinner probes; triangular probe; viscous sublayer; wall shear stress measurement; wall stress probe; Automotive components; Calibration; Mechanical variables measurement; Pressure measurement; Probes; Shape measurement; Size measurement; Stress measurement; Testing; Velocity measurement;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation in Aerospace Simulation Facilities, 1997. ICIASF '97 Record., International Congress on
  • Conference_Location
    Pacific Grove, CA
  • Print_ISBN
    0-7803-4167-8
  • Type

    conf

  • DOI
    10.1109/ICIASF.1997.644684
  • Filename
    644684