Buckling of Sandwich Cylinders Under Bending and Combined Bending and Axial Compression
- 1 July 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (7), 468-470
- https://doi.org/10.2514/8.2341
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Buckling of Sandwich Cylinders Under Axial CompressionJournal of the Aeronautical Sciences, 1951
- A Non‐linear Wing Theory and its Application to Rectangular Wings of Small Aspect RatioZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1939