Date of Award
12-1994
Document Type
Thesis
Degree Name
Master of Science
Department
Department of Aeronautics and Astronautics
Abstract
This study was carried out to investigate the elevated temperature behavior of the SiC-MAS5 cross- ply [0-90]4S ceramic matrix composite manufactured by Corning Inc. to fatigue with loading waveforms that combine the characteristics of stress rupture and high cycle fatigue. The test results were compiled in the form of S-N (cycles to failure), S-T (exposure time versus cycles to failure), S-S (energy exposure versus cycles to failure), normalized modulus degradation, strain progression, and hysteresis loop progression. From the mechanical behavior demonstrated by these curves, relationships between the effect of the environment and loading waveform were developed. In addition, a post-mortem SEM analysis of the fracture surface was conducted and the results compared to the mechanical behavior.
AFIT Designator
AFIT-GAE-ENY-94D-16
DTIC Accession Number
ADA289418
Recommended Citation
Grant, Scott A., "Fatigue Behavior of a Cross-Ply Ceramic Matrix Composite Subjected to Tension-Tension Cycling with Hold Time" (1994). Theses and Dissertations. 6342.
https://scholar.afit.edu/etd/6342
Included in
Aerospace Engineering Commons, Ceramic Materials Commons, Mechanics of Materials Commons