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
Link To Document :
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