Fatigue Life Prediction in Titanium Matrix Composites

1995 ◽  
Vol 117 (4) ◽  
pp. 440-447 ◽  
Author(s):  
T. Nicholas

Methods used for life prediction of titanium matrix composites under isothermal and thermomechanical (TMF) fatigue are reviewed. Models containing a single parameter are shown to have applicability only under limited conditions. Two models, a dominant damage and a life fraction model, demonstrate predictive capabilities over a broad range of loads, frequencies, temperatures, and TMF parameters. Relationships between the underlying fatigue mechanisms and the individual terms in the models are illustrated.

1998 ◽  
Vol 20 (2) ◽  
pp. 79 ◽  
Author(s):  
WS Johnson ◽  
JE Masters ◽  
DW Wilson ◽  
T Nicholas ◽  
JL Kroupa

2016 ◽  
Vol 51 (15) ◽  
pp. 2131-2141 ◽  
Author(s):  
Zheng Yuan ◽  
Robert Crouch ◽  
Jeff Wollschlager ◽  
Jacob Fish

Multiscale Designer, developed by Altair, has been studied for its suitability for fatigue life prediction of advanced composite aircraft structures made of polymer matrix composites. The extensive experimental data provided by the Air Force Research Laboratory have been utilized to characterize the linear, non-linear, monotonic, and cyclic loading properties of micro-constituents comprising the polymer matrix composite system. The characterized properties have been then utilized to predict fatigue life and residual strength and stiffness of the aerospace grade polymer matrix composites.


Sign in / Sign up

Export Citation Format

Share Document