GLTRS--Glenn
TITLE AND SUBTITLE:
In-Phase Thermomechanical Fatigue Mechanisms in an Unidirectional SCS-6/Ti 15-3 MMC

AUTHOR(S):
Golam M. Newaz and Bhaskar S. Majumdar

REPORT DATE:
June 1995

FUNDING NUMBERS:
WU-505-63-12
C-NAS3-26822

PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES):
Battelle Memorial Institute
505 King Avenue
Columbus, Ohio 43201

PERFORMING ORGANIZATION REPORT NUMBER:
E-9716

SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES):
National Aeronautics and Space Administration
Lewis Research Center
Cleveland, Ohio 44135-3191

REPORT TYPE AND DATES COVERED:
Final Contractor Report

SPONSORING/MONITORING AGENCY REPORT NUMBER:
NASA CR-195482

SUPPLEMENTARY NOTES:
Golam M. Newaz, Battelle Memorial Institute, 505 King Avenue, Columbus, Ohio 43201 (work funded by NASA Contract NAS3-26822), and Bhaskar S. Majumdar, Universal Energy Systems, 4401 Dayton-Xenia Rd., Dayton, Ohio 45432. Project Manager, Brad Lerch, Structures Division, NASA Lewis Research Center, organization code 5220,
(216) 433-5522.

ABSTRACT:
The objective of this investigation was to identify the inelastic deformation and damage mechanisms under in-phase (IP) thermomechanical fatigue (TMF) in a unidirectional SCS-6/Ti 15-3 metal matrix composite (MMC). Load-controlled IP TMF tests were conducted at 300-538 °C at various stress ranges in high-purity argon. A major emphasis of this work was to identify damage mechanism well before final fracture of specimens, rather than to generate life diagrams, to aid development of a realistic deformation/damage and life model.

SUBJECT TERMS:
Metal matrix composite; Fatigue; SiC/Ti-15-3; Deformation; Damage

NUMBER OF PAGES:
67

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