Effect of Buckling Modes on the Fatigue Life and Damage Tolerance of Stiffened StructuresThe postbuckling response and the collapse of composite specimens with a co-cured hat stringer are investigated experimentally and numerically. These specimens are designed to evaluate the postbuckling response and the effect of an embedded defect on the collapse load and the mode of failure. Tests performed using controlled conditions and detailed instrumentation demonstrate that the damage tolerance, fatigue life, and collapse loads are closely tied with the mode of the postbuckling deformation, which can be different between two nominally identical specimens. Modes that tend to open skin/stringer defects are the most damaging to the structure. However, skin/stringer bond defects can also propagate under shearing modes. In the proposed paper, the effects of initial shape imperfections on the postbuckling modes and the interaction between different postbuckling deformations and the propagation of skin/stringer bond defects under quasi-static or fatigue loads will be examined.
Document ID
20150006850
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Davila, Carlos G. (NASA Langley Research Center Hampton, VA, United States)
Bisagni, Chiara (California Univ., San Diego La Jolla, CA, United States)
Rose, Cheryl A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 28, 2015
Publication Date
January 5, 2015
Subject Category
Structural Mechanics
Report/Patent Number
NF1676L-19118Report Number: NF1676L-19118
Meeting Information
Meeting: AIAA SciTech 2015 Meeting
Location: Kissimmee, FL
Country: United States
Start Date: January 5, 2015
End Date: January 9, 2015
Sponsors: American Inst. of Aeronautics and Astronautics