Abstract
The present study concentrates on resin cracks in UD-layers of cross-ply laminates. The material T300 / 914C was tested mainly under T-fatigue, thermal cycling at space conditions and overheating, in order to analyse the damage mechanisms for resin layer cracks and their causes.
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Bibliography
W. Bergmann et al.: Mechanical Properties and Damage Mechnisms of CarbonfiberReinforced Composites–Compression Loading. DFVLR-FB 88–41, 1988, 262–293.
A. Höhn: Schichtrißbildung in Kreuzschichtlaminaten. Study work, T.U. Braunschweig, 1989.
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© 1990 Springer-Verlag Berlin, Heidelberg
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Eggers, H., Goetting, H.C., Hartung, W., Twardy, H. (1990). Matrix Cracking of Cross-ply Laminates under T-fatigue and Thermal Loading. In: Herrmann, K.P., Olesiak, Z.S. (eds) Thermal Effects in Fracture of Multiphase Materials. Lecture Notes in Engineering, vol 59. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-88479-5_17
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DOI: https://doi.org/10.1007/978-3-642-88479-5_17
Publisher Name: Springer, Berlin, Heidelberg
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