A study to determine the effect of glass compositional variations on vibration damping properties /
This report describes the results of an experimental investigation to determine the effects certain oxide additions have on the damping properties of a commercial glass (enamel) of known composition (Corning 0010) whose damping properties had previously been characterized. One of the aims of this in...
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| Corporate Authors: | , , |
| Other Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Wright-Patterson Air Force Base, Ohio :
Materials Laboratory, Air Force Wright Aeronautical Laboratory, Air Force Systems Command, United States Air Force,
1980.
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| Series: | AFWAL-TR (Air Force Wright Aeronautical Laboratories) ;
80-4061. |
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| Summary: | This report describes the results of an experimental investigation to determine the effects certain oxide additions have on the damping properties of a commercial glass (enamel) of known composition (Corning 0010) whose damping properties had previously been characterized. One of the aims of this investigation was to determine the effect the oxide additions had on the temperature at which peak damping occurred, singly and in combination. Past experience indicated the temperature of peak damping to be related to the viscosity of the glass. The results of this investigation indicated the temperature at which peak damping occurs (peak in the loss modulus curve) is related to the viscosity of the glass. |
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| Item Description: | "May 1980." ADA089499 (From http://www.dtic.mil). Research supported by the United States Air Force Wright Aeronautical Laboratory, and performed at the University of Dayton Research Institute. |
| Physical Description: | xii, 161 page : illustrations ; 28 cm. |
| Bibliography: | Includes bibliographical references (pages 160-161). |