NASA Technical Reports Server (NTRS) : Practical pdf

NASA Technical Reports Server (NTRS) : Practical_bookcover

NASA Technical Reports Server (NTRS) : Practical

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Four major areas of interest with respect to utilizing strain gages on carbon/carbon (with SiC surfaces) and titanium matrix composites are addressed. Strain gage and adhesive combinations on carbon/carbon (C/C) at temperatures from minus 190 C to to 540 C, half-bridge gaging for reducing apparent strain on C/C using Poisson’s ratio and bending configurations, a review of the ‘field installation’ techniques developed for gaging a C/C hypersonic generic elevon, and results of initial strain gaging efforts on titanium matrix composites are discussed. Current research in developing techniques for increasing the maximum temperature for strain gages on carbon/carbon are reviewed

  • Creator/s: NASA Technical Reports Server (NTRS
  • Date: 3/1/1991
  • Year: 1991
  • Book Topics/Themes: NASA Technical Reports Server (NTRS), ADHESION, ADHESIVES, HIGH TEMPERATURE, INSTALLING, METAL MATRIX COMPOSITES, SILICON CARBIDES, STRAIN GAGES, TITANIUM, BENDING, HYPERSONICS, POISSON RATIO, Moore, Thomas C., Sr

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