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Design and Testing of Honeycomb Sandwich Cylinders Under Axial CompressionExperimental results for 36" diameter honeycomb cylinders fabricated with thin (0.010") aluminum faces and cores prove that it is quite feasible to stabilize thin faces so they can be loaded Beyond the yield point. The effect of initial imperfections and the various modes of failure are discussed.
Document ID
19630000960
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
John H. Cunningham (Douglas Aircraft Co., Inc. Santa Monica, CA, United States)
Marcus J. Jacob (Douglas Aircraft Co., Inc. Santa Monica, CA, United States)
Date Acquired
August 1, 2013
Publication Date
October 24, 1962
Publication Information
Publication: Collected Papers on Stability of Shell Structures - 1962
Publisher: National Aeronautics and Space Administration
Volume: Technical Note: D-1510
Issue Publication Date: December 1, 1962
Subject Category
Thermodynamics And Combustion
Meeting Information
Meeting: NASA Symposium on Instability of Shell Structures
Location: Hampton, VA
Country: US
Start Date: October 24, 1962
End Date: October 25, 1962
Sponsors: Langley Research Center
Accession Number
63N10834
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
AXIAL COMPRESSION
HONEYCOMB
SHELL STABILITY
SANDWICH CONSTRUCTION

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