225 Time and Temperature Dependence on Flexural Fracture Behavior of Honeycomb Core Sandwich Panels
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概要
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Honeycomb core sandwich panels with the GFRP laminates as skin layer and aramid honeycomb core were employed for this study. The three point bending tests for the sandwich panels as well as the GFRP laminates were carried out at wide ranges of both deflection rate and temperature. The flexural strength for laminates and panel strongly depend on time and temperature. The time-temperature superposition principle holds for the flexural strength of the sandwich panel as well as GFRP laminates. The time-temperature shift factors for both strengths agreed well with each other in the temperature range of which the compressive fracture of GFRP occurred.
- 一般社団法人日本機械学会の論文
著者
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NAKADA Masayuki
Materials and Processing Research Center, NKK Corporation
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Miyano Yasusi
Materials System Research Lab. Kanazawa Institute Of Technology
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Miyano Yasushi
Materials System Reaearch Laboratory Kanazawa Institute Of Techology
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Mizotani Toru
Graduate School, Kanazawa Inst. of Tech.
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Mizotani Toru
Materials System Research Lab. Kanazawa Institute Of Technology
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Nakada Masayuki
Materials And Processing Research Center Nkk Corporation
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