Discrete element approach to flutter of skew panels with in-plane forces under yawed supersonic flow
- 1 November 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (11) , 2017-2022
- https://doi.org/10.2514/3.6040
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Application of matrix displacement methods in the study of panel flutter.AIAA Journal, 1969
- Finite elements applied to panel flutter.AIAA Journal, 1967
- Matrix displacement analysis of plates and shellsArchive of Applied Mechanics, 1966
- Flutter of Thin Plates under Combined Shear and Normal Edge ForcesAIAA Journal, 1963
- Flutter of Rectangular Simply Supported Panels at High Supersonic SpeedsJournal of the Aeronautical Sciences, 1957