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J. Aerosp. Technol. Manag. vol.4 número4

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Academic year: 2018

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Figure 1. DMA result for a standard sample at 11 Hz with 0.01% oscillatory strain at heating rate of 2 ºC/minutes.
Figure 4. Tan delta  versus  frequency for different temperatures at 0.5% strain.
Figure 6. Relaxation modulus  versus  time at different temperatures at 0.1% strain.
Figure 10. Relaxation modulus  versus  time for different strains at 35 ºC.
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