Subsonic Transient Lifting Surface Aerodynamics
- 1 January 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (1) , 44-50
- https://doi.org/10.2514/3.58748
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Active Flutter Control-An Adaptable Applicationto Wing/Store FlutterJournal of Aircraft, 1973
- An approximate true damping solution of the flutter equation by determinant iteration.Journal of Aircraft, 1971
- A rapid and stable subsonic collocation method for solving oscillatory lifting-surface problems by the use of quadrature integrationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.AIAA Journal, 1969
- A strip method for prediction of damping in subsonic wind tunnel andflight flutter tests.Journal of Aircraft, 1969
- A MORE REALISTIC METHOD FOR ROUTINE FLUTTER CALCULATIONSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- 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