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A Numerical Study on the Edgewise Compression Strength of Sandwich Structures with Facesheet-Core DisbondsDamage tolerant design approaches require determination of critical damage modes and flaw sizes in order to establish nondestructive evaluation detection requirements. A finite element model is developed to assess the effect of circular facesheet-core disbonds on the strength of sandwich specimens subjected to edgewise compressive loads for the purpose of predicting the critical flaw size for a variety of design parameters. Postbuckling analyses are conducted in which an initial imperfection is seeded using results from a linear buckling analysis. Both the virtual crack closure technique (VCCT) and cohesive elements are considered for modeling disbond growth. Predictions from analyses using the VCCT and analyses using cohesive elements are in good correlation. A series of parametric analyses are conducted to investigate the effect of core thickness and material, facesheet layup, facesheet-core interface properties, and curvature on the criticality of facesheet-core disbonds of various sizes. The results from these analyses provide a basis for determining the critical flaw size for facesheet-core disbonds subjected to edgewise compression loads and, therefore, nondestructive evaluation flaw detection requirements for this configuration.
Document ID
20170001031
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Bergan, Andrew C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
January 31, 2017
Publication Date
January 9, 2017
Subject Category
Spacecraft Design, Testing And Performance
Composite Materials
Structural Mechanics
Report/Patent Number
NF1676L-24620
Report Number: NF1676L-24620
Meeting Information
Meeting: AIAA SciTech 2017
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Composites, American Society of Mechanical Engineers, American Society of Civil Engineers, American Helicopter Society, Inc.
Funding Number(s)
WBS: WBS 826611.04.07.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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