Abstract:
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The Air Force sponsored flight tests using damage dosimeters, fabricated by The Boeing Company, to measure temperature and structural dynamic strains on B-52, F-15, and C-130 aircraft. The dosimeter measurements help diagnose difficult-to-analyze structural conditions, such as acoustics and high-cycle fatigue, and support the durability patch design process to repair secondary structure cracks. The dosimeter is a rugged, small, lightweight data acquisition unit that runs autonomously off of battery power. It measures three channels of strain at a rate up to 15 kilo-samples per second and one channel of temperature at a rate of 1.3 samples per second. The dosimeter acquires data above a programmer-defined root mean square (rms) strain threshold. It is currently programmed to store 42 time-history records (0.3 seconds each) and compute and store 29,544 third-octave spectra (18 bands each) in its 4-megabyte memory. LabVIEW virtual instruments (VIs) provide a quick look at the time-history and third-octave data, and stores mean, rms, and standard deviation values into a spreadsheet. This paper compares rms values computed from third-octave data with rms values from time-history data.
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