The development of a skin-friction balance to be used in a wind tunnel with heat-transfer conditions is described. The balance is a null-type device with a floating head element whose temperature can be maintained between 100K and 345K. This is accomplished with a cooled or heated jacket that is placed in direct contact with the friction element. At the desired element temperature the jacket is separated from the element and the shear-force data is taken. The balance was used in a Mach 5 supersonic flow with moderate heat-transfer rates. Shear forces ranging from 0.05 gm/sq cm to 1 gm/sq cm have been measured and higher ranges can be obtained by simply changing a coil spring. (Author)."18 June 1969".Includes bibliographical references (page...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
Skin friction and heat transfer data for hypersonic turbulent layer on flat plates, wind tunnel wall...
Skin-friction measurements are reported for high-enthalpy and high-Mach-number laminar, transitional...
Wall-temperature discontinuities can occur in skin-friction balance tests whenever a balance drag el...
The first part of this report describes the design and construction of a floating element skin frict...
A device has been developed to measure local skin friction on a flat plate by measuring the force ex...
The experience at LaRC with the University of Tennessee Space Institute skin friction balances is su...
The present report describes the design and construction of a floating-element skin-friction balance...
Embedded-wire skin-friction gages were tested in the Acoustic Research Tunnel (ART) and on a model i...
Research on force balance instrumentation to measure the skin friction of hypersonic vehicles at ext...
A device has been developed to measure local skin friction on a flat plate by measuring the force ex...
For a number of years now, experimenters have been making measurements of skin friction. Formerly, t...
Abstract: The method presented in NACA TN 2692 for evaluating the skin friction of a turbulent bound...
This study further developed and improved a miniature plastic cantilever floating element gauge for ...
Local heat-transfer rates on the surface of a heated flat plate at zero incidence to an air stream f...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
Skin friction and heat transfer data for hypersonic turbulent layer on flat plates, wind tunnel wall...
Skin-friction measurements are reported for high-enthalpy and high-Mach-number laminar, transitional...
Wall-temperature discontinuities can occur in skin-friction balance tests whenever a balance drag el...
The first part of this report describes the design and construction of a floating element skin frict...
A device has been developed to measure local skin friction on a flat plate by measuring the force ex...
The experience at LaRC with the University of Tennessee Space Institute skin friction balances is su...
The present report describes the design and construction of a floating-element skin-friction balance...
Embedded-wire skin-friction gages were tested in the Acoustic Research Tunnel (ART) and on a model i...
Research on force balance instrumentation to measure the skin friction of hypersonic vehicles at ext...
A device has been developed to measure local skin friction on a flat plate by measuring the force ex...
For a number of years now, experimenters have been making measurements of skin friction. Formerly, t...
Abstract: The method presented in NACA TN 2692 for evaluating the skin friction of a turbulent bound...
This study further developed and improved a miniature plastic cantilever floating element gauge for ...
Local heat-transfer rates on the surface of a heated flat plate at zero incidence to an air stream f...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
Skin friction and heat transfer data for hypersonic turbulent layer on flat plates, wind tunnel wall...
Skin-friction measurements are reported for high-enthalpy and high-Mach-number laminar, transitional...