THE EFFECT OF A CAVITY ON PANEL VIBRATION
Authors:
- 1 February 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (2) , 476-477
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- The Buckling of Thin Cylindrical Shells Under Axial CompressionJournal of the Aeronautical Sciences, 1941