Adhesive-bonded composite joint analysis with delaminated surface ply using strain-energy release rate

Journal of Aircraft

Volumn 49, Issue 2, 2012, Pages 503-520

  Chadegani, Alireza ^a,b   Yang, Chihdar ^a   Smeltzer, Stanley S ^c  

^a Wichita State University   (United States)

^b VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVES; ANALYTICAL MODELS; COMPUTATION THEORY; CRACK CLOSURE; DIFFERENTIAL EQUATIONS; ENERGY RELEASE RATE; JOINTS (STRUCTURAL COMPONENTS); PLATES (STRUCTURAL COMPONENTS); SHEAR DEFORMATION; STRAIN ENERGY; STRAIN RATE; STRESS ANALYSIS; STRESS CONCENTRATION;

ADHESIVELY BONDED COMPOSITE JOINTS; DELAMINATED SURFACES; DISPLACEMENTS FIELDS; FIELD DISPLACEMENTS; FIRST-ORDER SHEAR DEFORMATION THEORY; INTERLAMINAR CRACKS; SECOND-ORDER DIFFERENTIAL EQUATION; SYMBOLIC COMPUTATION;

FINITE ELEMENT METHOD;

EID: 84859337849     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.C031516     Document Type: Article

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