Determination of Principal Properties of 'E' Fiber-Glass High Temperature Epoxy Laminates for Aircraft

摘要

A test program was conducted to develop mechanical strength data on ECDE 7581 glass fabric impregnated with F161 resin. This data is to be used in the new revision of MIL-HDBK-17. The properties determined were tensile, compressive and shear strengths and stiffnesses and Poisson's ratios over the temperature range of -65F to 450F. The results are presented in graphical, tabular, and summary forms. (Author)