Accession Number:

ADA162370

Title:

Delamination Buckling and Growth of Flat Composite Structural Elements.

Descriptive Note:

Annual rept. 1 Jul 83-31 Aug 84,

Corporate Author:

GEORGIA INST OF TECH ATLANTA SCHOOL OF ENGINEERING SCIENCE AND MECHANICS

Personal Author(s):

Report Date:

1984-09-01

Pagination or Media Count:

83.0

Abstract:

Delamination buckling and growth of flat composite structural elements is presented with sufficient detail. The mathematical model for the phenomena are developed and solved. The emphasis of the analysis is to establish the load carrying capability damage tolerance of the delaminated structural element and to identify the most influencing structural parameters. Two important parameters have a governing influence on the behavior of the delaminated damaged element the size of the delamination and its position in the laminate, especially its distance from the surface. Depending on these two parameters, the damage tolerance of the laminate is either governed by delamination buckling or by the fracture toughness of the material delamination growth. Keywords Laminated plates Delamination buckling Delamination growth Damage tolerance.

Subject Categories:

  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE