Composite structure global fracture toughness via computational simulation

Computers and Structures

Volumn 37, Issue 2, 1990, Pages

  Minnetyan, L ^a   Murthy, P L N ^b   Chamis, C C ^b  

^a CLARKSON UNIVERSITY   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES--MATERIALS; COMPUTER SIMULATION; LAMINATED PRODUCTS--COMPOSITES; PLASTICS LAMINATES--FIBER REINFORCEMENT; PLATES--COMPOSITE;

DELAMINATION; FUNDAMENTAL BUCKLING LOAD; GLOBAL FRACTURE TOUGHNESS; MULTIPLY FIBER COMPOSITE LAMINATES; NATURAL FREQUENCIES; STRUCTURAL DEGRADATION;

COMPOSITE STRUCTURES;

EID: 0025640147     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/0045-7949(90)90399-M     Document Type: Article

References (10)

1. Composite durability structural analysis
2. Progressive fracture of fiber composites
3. Structural behavior of composites with progressive fracture
4. Progression of damage and fracture in composites under dynamic loading
5. ICAN: integrated composites analyzer
6. Integrated composite analyzer (ICAN): users and programmers manual
7. Composite interlaminar fracture toughness: 3-D finite element modeling for mixed mode I, II, and III fracture
8. Strain energy release rates of composite interlaminar end-notch and mixed mode fracture: a sublaminate/ply level analysis and a computer code
9. Finite element substructuring methods for composite mechanics