Advances in fan and compressor blade flutter analysis and predictions
- 1 April 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 12 (4), 325-332
- https://doi.org/10.2514/3.44451
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Supersonic Unstalled Flutter In Fan Rotors; Analytical and Experimental ResultsJournal of Engineering for Power, 1974
- The Unsteady Aerodynamics of a Finite Supersonic Cascade With Subsonic Axial FlowJournal of Applied Mechanics, 1973
- Coupled Blade-Disk-Shroud Flutter Instabilities in Turbojet Engine RotorsJournal of Engineering for Power, 1967
- Aerodynamic forces on an oscillating aerofoil fitted with a spoilerProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1957