Aerodynamic Flutter Derivatives for a Flexible Wing with Supersonic and Subsonic Edges
- 1 October 1955
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 22 (10), 693-700
- https://doi.org/10.2514/8.3436
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Generalized Aerodynamic Forces on the Delta Wing with Supersonic Leading EdgesJournal of the Aeronautical Sciences, 1954
- Influence of Primary Creep on Column BucklingJournal of Applied Mechanics, 1954
- Forty-First Wilbur Wright Memorial Lecture: Buckling and StabilityJournal of the Royal Aeronautical Society, 1954
- On the Nonexistence of a Finite Critical Time for Linear Viscoelastic ColumnsJournal of the Aeronautical Sciences, 1953
- Creep Deflections in ColumnsJournal of Applied Physics, 1947