Design and analysis of test coupons for composite blade repairs

Composite Structures

Volumn 37, Issue 2, 1997, Pages 185-193

  Oztelcan, C ^a   Ochoa, O O ^b   Martin, J ^c   Sem, K ^c  

^a INTEL CORPORATION   (United States)

^b Texas AandM University   (United States)

^c BELL HELICOPTER TEXTRON INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMPOSITE MATERIALS; FINITE ELEMENT METHOD; GEOMETRY; LOADS (FORCES); MATERIALS TESTING; MATHEMATICAL MODELS; REPAIR; STRAIN;

COMPOSITE BLADE; GLOBAL BLADE MODEL; SCARF PRECURED PATCH REPAIR; STATIC LOADING CONDITION; STRAIN DISTRIBUTION; TENSILE LOAD; TEST COUPONS; UNIAXIAL COMPRESSIVE LOAD;

COMPOSITE STRUCTURES;

EID: 0031073560     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(97)80011-6     Document Type: Article

References (2)

1. Kline, R. A., Stress analysis of adhesively bonded joints. Engineering Mechanics Department, General Motors Research Laboratories, Warren, MI, 1988.
2. Messler, R. W., Joining of Advance Materials. Butterworth-Heineman Stoneham, MA, 02180, 1993.