EFFECTS OF ORTHOTROPICITY ORIENTATION ON SUPERSONIC PANEL FLUTTER
- 1 September 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (9) , 2180-2182
- https://doi.org/10.2514/3.2033
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- EFFECTIVE DISPLACEMENT THICKNESS FOR BOUNDARY LAYERS WITH SURFACE MASS TRANSFERAIAA Journal, 1963
- An Introduction to Applied Anisotropic ElasticityPhysics Today, 1961
- Flutter of Rectangular Simply Supported Panels at High Supersonic SpeedsJournal of the Aeronautical Sciences, 1957