Life Prediction, Durability, and Damage
Tolerance of High Temperature Polymer Composite Structures in Aerospace Applications
S. R. Patel and S. W. Case
This paper presents the results to date of an ongoing study on the
effects of temperature and mechanical fatigue on the residual strength of a five-harness
satin weave reinforced polymeric composite. Unaged specimens underwent mechanical fatigue
testing at room temperature and at 120°C. Tests were interrupted at two different stages
of fatigue life to monitor damage and to obtain stiffness changes and residual strengths.
Initial material strength and stiffness were measured to be approximately 738 MPa and 65.6
GPa, respectively, at both temperatures. As a result of fatigue loading (R = 0.1) at 455
MPa and 10 Hz, the strengths remained unchanged, but the residual stiffness decreased at
both temperatures, particularly at 120°C. Data collected thus far show that temperature
has a significant impact on fatigue life.