UNIRED THEORY FOR THE BENDING AND BUCKLING OF SANDWICH SHELLS - APPLICATION TO AXIALLY COMPRESSED CIRCULAR CYLINTRICAL SHELLS
- 29 March 1967
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- UNIRED THEORY FOR THE BENDING AND BUCKLING OF SANDWICH SHELLS - APPLICATION TO AXIALLY COMPRESSED CIRCULAR CYLINTRICAL SHELLSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- General instability and face wrinkling of sandwich plates - Unified theory and applicationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966