Buckling of Orthotropic Sandwich Cylinders Under Axial Compression and Bending
Author:
Affiliation:
1. University of Kansas, Lawrence, Kan.
2. University of Oklahoma, Norman, Okla.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.59221
Reference24 articles.
1. UNIRED THEORY FOR THE BENDING AND BUCKLING OF SANDWICH SHELLS - APPLICATION TO AXIALLY COMPRESSED CIRCULAR CYLINTRICAL SHELLS
2. Buckling of Sandwich Cylinders Under Combined Compression, Torsion, and Bending Loads
3. Buckling of cylindrical and conical sandwich shells with orthotropicfacings.
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