An experimental study was conducted to determine the effects of ply thickness in composite laminates on thermally induced cracking and changes in the coefficient of thermal expansion (CTE). After a few thermal cycles, laminates with thick-plies cracked, resulting in large changes in CTE. CTE's of the thin-ply laminates were unaffected by microcracking during the first 500 thermal cycles, whereas, the CTE's of the thick-ply laminates changed significantly. After about 1500 cycles, microdamage had also reduced the CTE of the thin-ply laminates to a value of about half of their initial value
Carbon fiber reinforced polymer composites have been widely used in space industries for manufacturi...
The effects of thermal and mechanical fatigue on the flexural strength of G40-600/PMR-15 cross-ply l...
Conventional aerospace composites are strong and stiff in the directions parallel to the carbon fibe...
Carbon fiber composites are materials of great interest to the aerospace industry because of their l...
State-of-the-art, high temperature polyimide matrix composites, reinforced with continuous graphite ...
Composites used in space structures are exposed to both extremes in temperature and applied mechanic...
Graphite-epoxy laminates were thermally cycled to determine the effects of thermal cycles on tensile...
The thermal expansion of three epoxy-matrix composites, a polyimide-matrix composite and a borosilic...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
Thermal expansion data for several composite materials, including generic epoxy resins, various grap...
A general analysis method is presented to predict matrix cracks in all plies of a composite laminate...
This report summarizes the work done in the period February 1993 through July 1993 on the 'Predictio...
Carbon fiber-reinforced polymer material has been widely used in space/aerospace industries for manu...
This paper compares the thermal properties of thick (2.125 ") versus thin (0.212 ") lamina...
The effect of thermal-cycling-induced microcracking in fiber-reinforced polymer matrix composites is...
Carbon fiber reinforced polymer composites have been widely used in space industries for manufacturi...
The effects of thermal and mechanical fatigue on the flexural strength of G40-600/PMR-15 cross-ply l...
Conventional aerospace composites are strong and stiff in the directions parallel to the carbon fibe...
Carbon fiber composites are materials of great interest to the aerospace industry because of their l...
State-of-the-art, high temperature polyimide matrix composites, reinforced with continuous graphite ...
Composites used in space structures are exposed to both extremes in temperature and applied mechanic...
Graphite-epoxy laminates were thermally cycled to determine the effects of thermal cycles on tensile...
The thermal expansion of three epoxy-matrix composites, a polyimide-matrix composite and a borosilic...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
Thermal expansion data for several composite materials, including generic epoxy resins, various grap...
A general analysis method is presented to predict matrix cracks in all plies of a composite laminate...
This report summarizes the work done in the period February 1993 through July 1993 on the 'Predictio...
Carbon fiber-reinforced polymer material has been widely used in space/aerospace industries for manu...
This paper compares the thermal properties of thick (2.125 ") versus thin (0.212 ") lamina...
The effect of thermal-cycling-induced microcracking in fiber-reinforced polymer matrix composites is...
Carbon fiber reinforced polymer composites have been widely used in space industries for manufacturi...
The effects of thermal and mechanical fatigue on the flexural strength of G40-600/PMR-15 cross-ply l...
Conventional aerospace composites are strong and stiff in the directions parallel to the carbon fibe...