A Comparison of Methods for the Analysis of Wing-Tail Interaction Flutter
- 1 May 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (5) , 361-367
- https://doi.org/10.2514/3.59109
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Flutter induced by aerodynamic interference between wing and tailJournal of Aircraft, 1970
- Modified-strip-analysis method for predicting wing flutter at subsonic to hypersonic speeds.Journal of Aircraft, 1966
- COLLOCATION METHOD FOR CALCULATING THE AERODYNAMIC PRESSURE DISTRIBUTIONS ON A LIFTING SURFACE OSCILLATING IN SUBSONIC COMPRESSIBLE FLOWPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- New directions in lifting surface theoryAIAA Journal, 1965