Buckling Testing and Analysis of Honeycomb Sandwich Panel Arc Segments of a Full-Scale Fairing Barrel: Comparison of In- and Out-of-Autoclave Facesheet Configurations
Author:
Affiliation:
1. NASA Glenn Research Center
2. Vantage Partners, LLC
3. ZIN Technologies, Inc.
4. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-1052
Reference25 articles.
1. Validation of Lower-Bound Estimates for Compression-Loaded Cylindrical Shells
2. Developing the Next Generation Shell Buckling Design Factors and Technologies
3. The Effects of Geometric and Loading Imperfections on the Response and Lower-Bound Buckling Load of a Compression-Loaded Cylindrical Shell
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3. Cohesive zone modeling for mode I facesheet to core delamination of sandwich panels accounting for fiber bridging;Composite Structures;2018-01
4. Post-buckling Analysis of Curved Honeycomb Sandwhich Panels Containing Interfacial Disbonds;57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2016-01-01
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