An Exact Solution for the Buckling Load of Flat Sandwich Panels with Loaded Edges Clamped
- 1 September 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (9) , 605-612
- https://doi.org/10.2514/8.2761
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- On the Lift and Circulation of Airfoils in Some Unsteady-Flow ProblemsJournal of the Aeronautical Sciences, 1952
- Tables of the Theodorsen Circulation Function for Generalized MotionJournal of the Aeronautical Sciences, 1951