Role of weak interface to retain high strength of fiber in monofilamentary SiC fiber/titanium-aluminide composite

Composite Interfaces

Volumn 4, Issue 3, 1996, Pages 157-168

  Ochiai, S ^a   Inoue, T ^a   Hojo, M ^a   Dudek, H J ^b   Leucht, R ^b  

^a KYOTO UNIVERSITY   (Japan)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

Crack blunting; Energy release rate; Interface; Monofilamentary composite; Silicon carbide; Tensile strength; Titanium aluminide

Indexed keywords

CRACKS; FRACTURE; INTERFACES (MATERIALS); INTERMETALLICS; SILICON CARBIDE; SPUTTERING; STRESS CONCENTRATION; SURFACE PHENOMENA; TENSILE STRENGTH; TENSILE TESTING;

CRACK BLUNTING; ENERGY RELEASE RATE; FRACTURE MECHANICAL ANALYSIS; INTERFACIAL DEBONDING; TITANIUM ALUMINIDE;

METALLIC MATRIX COMPOSITES;

EID: 0030387250     PISSN: 09276440     EISSN: 15685543     Source Type: Journal    
DOI: 10.1163/156855496X00236     Document Type: Article

References (5)

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3. J. M. Hedgepeth, NASA Technical Note D-882, (1961).
4. J. A. Narin, J. Compos. Mater. 22, 561 (1988).
5. S. Ochiai, K. Schulte and P. W. M. Peters, Compos. Set. Techn. 41, 237 (1991).