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
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