This study investigates the accuracy of spatially resolved skin friction velocity ut measurements using a large number of Irwin sensors (Irwin, 1981). A fast and simple procedure to calibrate the sensors against a two-component hot-film anemometer is introduced which leads to a universal calibration function that can then be used for all sensors. Insignificantly lower accuracies are obtained using the universal calibration function instead of individual calibration functions for each sensor. The overall accuracy of the skin friction velocity measurements averages about ±5% for ut>0.13 m s-1 and decreases strongly to ±20% at lower ut. The main sources of errors are as follows: (i) deviations from flush mounting of the sensors with the wal...
An accurate determination of friction velocity u ^ or, alterna-tively, of wall shear stress T „ = p...
Baronti-Libby transformation and Preston tube calibrations used to determine skin friction from turb...
Accurate skin friction measurements are indispensable in the design of more efficient aerodynamic ve...
A device has been developed to measure local skin friction on a flat plate by measuring the force ex...
Recent improvements in three techniques for measuring skin friction in two- and three-dimensional tu...
Embedded-wire skin-friction gages were tested in the Acoustic Research Tunnel (ART) and on a model i...
Experimental Results Of Mean Surface Skin Friction Using Hot-Films On A NACA 0012 Airfoil At Low Spe...
The first part of this report describes the design and construction of a floating element skin frict...
The present report describes the design and construction of a floating-element skin-friction balance...
The purpose of this study was to assess the feasibility of using flush-mounted surface hot-film sens...
A device has been developed to measure local skin friction on a flat plate by measuring the force ex...
A probe for wall shear stress measurements in nominally 2-D flows has been developed and tested. In...
Wall-temperature discontinuities can occur in skin-friction balance tests whenever a balance drag el...
Indirect methods to estimate surface shear stress are commonly used to characterise rough-wall bound...
The present work delivers a versatile, accurate and reliable wind tunnel facility that is particular...
An accurate determination of friction velocity u ^ or, alterna-tively, of wall shear stress T „ = p...
Baronti-Libby transformation and Preston tube calibrations used to determine skin friction from turb...
Accurate skin friction measurements are indispensable in the design of more efficient aerodynamic ve...
A device has been developed to measure local skin friction on a flat plate by measuring the force ex...
Recent improvements in three techniques for measuring skin friction in two- and three-dimensional tu...
Embedded-wire skin-friction gages were tested in the Acoustic Research Tunnel (ART) and on a model i...
Experimental Results Of Mean Surface Skin Friction Using Hot-Films On A NACA 0012 Airfoil At Low Spe...
The first part of this report describes the design and construction of a floating element skin frict...
The present report describes the design and construction of a floating-element skin-friction balance...
The purpose of this study was to assess the feasibility of using flush-mounted surface hot-film sens...
A device has been developed to measure local skin friction on a flat plate by measuring the force ex...
A probe for wall shear stress measurements in nominally 2-D flows has been developed and tested. In...
Wall-temperature discontinuities can occur in skin-friction balance tests whenever a balance drag el...
Indirect methods to estimate surface shear stress are commonly used to characterise rough-wall bound...
The present work delivers a versatile, accurate and reliable wind tunnel facility that is particular...
An accurate determination of friction velocity u ^ or, alterna-tively, of wall shear stress T „ = p...
Baronti-Libby transformation and Preston tube calibrations used to determine skin friction from turb...
Accurate skin friction measurements are indispensable in the design of more efficient aerodynamic ve...