Buckling initiation and disbond growth in adhesively bonded composite flanges

44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Volumn , Issue , 2003, Pages

  Kim, Hyonny ^a   Kwon, Hyukbong ^a   Keune, John ^a  

^a Purdue University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVELY BONDED; CLOSED FORM; DISBOND; GROWTH INITIATION; PREDICTIVE CAPABILITIES; SANDWICH PANEL; THEORETICAL MODELING;

FLANGES; STRUCTURAL DYNAMICS;

BUCKLING;

EID: 84896880515     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

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3. rd Structures, Structural Dynamics, and Materials Conference, Denver, CO, April 22-25, 2002.
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5. st Structures, Structural Dynamics, and Materials Conference, Seattle, WA, May 12-14, 1980, pp. 187-193.
6. Speir, E. E., Arnold, R. R., and Kedward, K. T., "Stability Critical Compression Members, " Handbook of Composites, Vol. 2, Ch. 11, Edited by C. T. Herakovich and Y. M. Tarnopol'skii, 1989.
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8. Chai, H. and Babcock, C.D., "Two-Dimensional Modelling of Compressive Failure in Delaminated Laminates, " Journal of Composite Materials, Vol. 19, 1985, pp. 67-98.
9. American Society for Testing and Materials, "Standard Test Method for Mode I Interlaminar Fracture Toughness of Unidirectional Fiber-Reinforced Polymer Matrix composites, " ASTM D5528, 2002.