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An investigation of larger scale coherent structures in fully developed turbulent boundary layersHutchins, Nick January 2003 (has links)
No description available.
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Study of A Direct Measuring Skin Friction Gage with Rubber Compounds for DampingMagill, Samantha Anne 11 August 1999 (has links)
A study was conducted on the measurement of skin friction, the least under-stood component of drag. Skin friction is considered the "last frontier" in drag reduction for supersonic flight, but to understand skin friction, it must be accurately measured. This study utilized the direct measuring technique for skin friction. A small de-vice, termed a skin friction gage, measures the stress on a cantilever beam topped with a movable surface piece as a shear flow passes over the flush surface. The improvement of these devices for various flow fields is ongoing. A problem that arose with many designs was leakage of a gap-filling liquid. The typical direct measuring skin friction gage uses oil in a gap between the cantilever beam and the encasement to dampen vibrations, to create an even flow over the surface, and for temperature compensation. In high speed testing the oil leaks out; therefore, a gage with rubber to fill the gap instead of oil was introduced
This study employed a finite element method model to fully understand the strains involved with the rubber and the skin friction gage. The development of a calibration device, called the Calibration Rig, for the rubber skin friction gages was constructed. The Calibration Rig was successful, but deemed to be more cumbersome than initially expected. This led to the development of a thin rubber sheet to cover the face of the gage instead of rubber filling the entire gap. More finite element method modeling was done to finalize the design of a gage with a rubber sheet. The design consisted of a plastic skin friction gage with an approximately 0.015 in. thick rubber sheet, a 0.0625 in. wide gap between the floating head on the cantilever beam and the encasement to be filled with oil, and semi-conductor strain gages to measure the beam deflection.
Vibration tests were performed to determine if the rubber sheet produced the required damping. These tests were successful, and so much so, that the oil for damping was not necessary. However, supersonic wind tunnel tests at Mach 2.4 which were done at Virginia Polytechnic Institute and State University, initially yielded unfavorable results. The rubber sheet failed during the violent process of starting and unstarting of the tunnel. More study on the adhesive mounting of the rubber sheet to the skin friction gage face is needed. / Master of Science
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The theory and application of heated films for the measurement of skin frictionMathews, J. January 1985 (has links)
The use of hot surface films for measuring skin friction is examined. It is shown that all existing theories, which neglect heat conduction within the substrate, are inadequate in predicting the variation of heat loss from the film with skin friction. A more physically realistic theory is presented which accounts for the conductive and convective heat transfer into the flow and also heat conduction within the substrate. This leads to a more general relationship between skin friction and heat loss from the film. Experiments conducted in flat plate laminar and turbulent boundary layer flow show that this relationship is more accurate than previous forms. The time and temperature dependence of the heat loss from the hot film are also explored theoretically and experi- mentally. The effect of surface misalignment of the film is shown to alter significantly the convective heat transfer. This effect is more pronounced in laminar flow than in turbulent flow. Using a glue-on hot film probe, calibrations relating the heat loss to skin friction were found to be different in laminar and turbulent flow. An experimental operating procedure for the use of hot surface films for measuring skin friction is proposed which significantly increases the accuracy of the technique.
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An experimental study of skin friction on a stationary flat surface in contact with vortex flowHuntley, James Richard 08 1900 (has links)
No description available.
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An actively cooled floating element skin friction balance for direct measurement in high enthalpy supersonic flows /Chadwick, Kenneth Michael, January 1992 (has links)
Thesis (Ph. D.)--Virginia Polytechnic Institute and State University, 1992. / Vita. Abstract. Includes bibliographical references (leaves 67-71). Also available via the Internet.
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Development of a cantilever beam, capacitive sensing, skin friction gage and supporting instrumentation for measurements /Horvath, Istvan. January 1993 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1993. / Vita. Also available via the Internet.
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Floating head skin friction gage measurements in supersonic flows /Lattimer, Brian Y., January 1993 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1993. / Vita. Abstract. Includes bibliographical references (leaves 122-123). Also available via the Internet.
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Heat transfer in compressible laminar boundary-layersLal, Shankar. January 1955 (has links)
Thesis--California Institute of Technology, 1955. / Also issued in print.
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The development of instrumentation for the support of skin friction and heat flux measurements /Putz, John M. January 1991 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1991. / Vita. Abstract. Includes bibliographical references (107-110). Also available via the Internet.
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Surface flow measurements of supersonic impinging microjetsDavy, Charney A. Alvi, Farrukh S. January 2003 (has links)
Thesis (Ph. D.)--Florida State University, 2003. / Advisor: Dr. Farrukh S. Alvi, Florida State University, FAMU - FSU College of Engineering, Dept. of Mechanical Engineering. Title and description from dissertation home page (Aug. 27, 2004). Includes bibliographical references.
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