Investigations Concerning the Coupled Wing-Fuselage-Tail Flutter Phenomenon
- 1 January 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 9 (1) , 48-54
- https://doi.org/10.2514/3.58935
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Application of the Doublet-Lattice Method to Nonplanar Configurations in Subsonic FlowJournal of Aircraft, 1971
- A Comparison of Methods for the Analysis of Wing-Tail Interaction FlutterJournal of Aircraft, 1971
- Flutter induced by aerodynamic interference between wing and tailJournal of Aircraft, 1970
- A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.AIAA Journal, 1969
- Numerical lifting-surface theory - Problems and progress.AIAA Journal, 1968
- New directions in lifting surface theoryAIAA Journal, 1965
- On the Calculation of Natural Modes of Free-Free StructuresJournal of the Aerospace Sciences, 1961
- Dynamics of Flight: Stability and ControlPhysics Today, 1959