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Increasing the sensitivity of the strain gage measurements by using pulsed inputsVail, Charles David, 1919- January 1952 (has links)
No description available.
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Investigation and design of a torquemeter using SR-4 strain gagesReece, Carroll Kent January 2011 (has links)
Digitized by Kansas State University Libraries
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A STRESS MEASURING DEVICE UTILIZING THE PIEZOTHERMAL EFFECTLinville, Frank Allison, 1916- January 1964 (has links)
No description available.
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The development of a photoelastic strain gauge to determine the principal strains directlyGarner, Edward Rogers, 1938- January 1965 (has links)
No description available.
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Studies relating to abutment stresses for mines.Udd, J. E. (John E.) January 1969 (has links)
No description available.
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Strain gauge measurements of blade resonance using eddy current excitation in a vacuum spin pit /Russell, Scott A. January 2002 (has links) (PDF)
Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, September 2002. / Thesis advisor(s): Raymond P. Shreeve, Garth V. Hobson. Includes bibliographical references (p. 93). Also available online.
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Studies relating to abutment stresses for mines.Udd, J. E. (John E.) January 1969 (has links)
No description available.
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Development of a five-component strain-gauge balance for the DSTO water tunnelErm, Lincoln P. Ferrarotto, Phil. January 2009 (has links) (PDF)
Mode of access: Internet via World Wide Web. Available at http://hdl.handle.net/1947/10033. / "November 2009". Available on the DSTO website as at DSTO at :http://dspace.dsto.defence.gov.au/dspace/bitstream/1947/10033/1/DSTO-GD-0597%20PR.pdf
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The design of skin friction gages for measurements in high-speed, short-duration flows /Busic, John F., January 1992 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1992. / Vita. Abstract. Includes bibliographical references (leaf 113). Also available via the Internet.
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Design and development of a three component strain gauge wind tunnel balancePieterse, Frederik Francois 05 September 2012 (has links)
M.Phil. / In today's world with its competitive environment there is a need to shorten product development time by using CFD (Computational Fluid Dynamics) to design an object for example a car, aeroplane or missile and to predict the forces that the wind will have on the object (design). To evaluate the correctness of the CFD results, the design or a scale model of the design must be tested in a wind tunnel by using a force balance. The wind tunnel balance is an apparatus used in the designing and testing of wings, shapes and profiles. In general a balance can be used in all aerodynamic designs to determine the forces on an object when it is moving through air. The aim of this project was to design and manufacture a three-component external balance for a low-speed wind tunnel using an axiomatic design method. It also covers the installation of the external wind tunnel balance to a wind tunnel with a computerized data acquisition capturing system, and performance evaluation of the wind tunnel balance.
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