Buckling of a tension panel containing a circular hole.
- 1 October 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (10) , 2012-2014
- https://doi.org/10.2514/3.4918
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Numerical solution of the boundary-layer equations.AIAA Journal, 1967
- Approximate solution of second-order boundary- layer equations.AIAA Journal, 1965
- Machine calculation of compressible laminar boundary layersAIAA Journal, 1965
- On the buckling under tension of a membrane containing holesJournal of Applied Mathematics and Mechanics, 1963
- Nonsimilar Solutions of the Compressible-Laminar Boundary-Layer Equations With Applications to the Upstream-Transpiration Cooling ProblemJournal of the Aerospace Sciences, 1961
- Laminar boundary-layer flow near separation with and without suctionPhilosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences, 1960