Curing Pressure Influence of Out-of-Autoclave Processing on Structural Composites for Commercial Aviation

<table>Stress-strain comparison of CFRP specimens manufactured under 0, 30, 50, and 70 psi derived from flexural testing.</table>

Advances in Materials Science and Engineering

Figure 15: Curing Pressure Influence of Out-of-Autoclave Processing on Structural Composites for Commercial Aviation 