An approximate true damping solution of the flutter equation by determinant iteration.
- 1 November 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (11) , 885-889
- https://doi.org/10.2514/3.44311
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- 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
- Graphical technique for analyzing marginally stable dynamic systemsJournal of Aircraft, 1964
- Theodorsen's Circulation Function for Generalized MotionJournal of the Aeronautical Sciences, 1952
- Generalization of the Theodorsen Function to Stable OscillationsJournal of the Aeronautical Sciences, 1952
- Tables of the Theodorsen Circulation Function for Generalized MotionJournal of the Aeronautical Sciences, 1951