Accession Number : ADA306410

Title :   Thermo-Mechanical Fatigue Behavior of Cross-Ply Ceramic Matrix Composite UnderTension-Tension Loading.

Descriptive Note : Master's thesis,

Corporate Author : AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH

Personal Author(s) : Allen, Dana G.

PDF Url : ADA306410

Report Date : DEC 1995

Pagination or Media Count : 146

Abstract : The purpose of this study was to investigate the combined effect of cyclic temperature and loading on the fatigue life of a ceramic matrix composite with a cross ply lay-up. The material used in this study was a potassium borosilicate glass (BSG) doped magnesium aluminosilicate (MAS) cordierite matrix reinforced with Nicalon (silicon carbide, SiC) fibers in a (O/90)4s lay-up. Thermomechanical fatigue (TMF) tests were performed with a period of 180 seconds/cycle, or 0.00556 Hz, and a triangular wave-form. The temperature was cycled between 566 C and l093 C, and the stress levels varied between 60 MPa and 145 MPa. All tests involved tension-tension cycling with a stress ratio of 0.1. These two temperatures and the stress ratio were chosen to correspond with previous studies on this material. Six tests were performed under in-phase TMF conditions, and five tests were performed out-of-phase TMF condition. Four fatigue tests were performed isothermally at 566 C, and three more at l093 C. Monotonic tests were also performed at room temperature, 566 C and 1093 C. Load and strain data were measured during all tests. This data was then used to get histories for maximum strain, minimum strain and strain range, modulus degradation, stress-strain hysteresis loops, and fatigue life curves. Post-mortem fractographic analysis, with optical and scanning electric microscopes, was also performed on the specimen. Damage and fracture mechanisms were thus determined. These results indicate a much higher damage for thermo-mechanical fatigue than for high temperature isothermal mechanical fatigue, with the out-of-phase TMF being much higher than the in-phase TMF. By comparing with previous data, it is shown that frequency has no effect, thus the damage is a time dependent phenomenon involving environmentally assisted crack growth and fiber-matrix debonding.

Descriptors :   *THERMOMECHANICS, *CERAMIC MATRIX COMPOSITES, *CERAMIC MATERIALS, *THERMAL FATIGUE, STRESS STRAIN RELATIONS, OPTICAL PROPERTIES, TENSILE STRESS, THESES, STRAIN(MECHANICS), FRACTURE(MECHANICS), CRACK PROPAGATION, FATIGUE(MECHANICS), SILICON CARBIDES, BORON OXIDES.

Subject Categories : Ceramics, Refractories and Glass
      Laminates and Composite Materials
      Thermodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE