The Design and Testing of Supersonic Flutter Models
- 1 June 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (6) , 530-542
- https://doi.org/10.2514/8.3602
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- The Compressible Boundary LayerJournal of the Aeronautical Sciences, 1952
- Turbulent Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1951