Flutter and Response of a Mistuned Cascade in Incompressible Flow
- 1 August 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (8), 1120-1127
- https://doi.org/10.2514/3.51172
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Coupled Bending-Torsion Flutter in CascadesAIAA Journal, 1980
- Unsteady Flow in a Supersonic Cascade with Subsonic Leading-Edge LocusAIAA Journal, 1978
- Influence of the material of the rotor blades of an axial-flow compressor under flutter initiating conditionsStrength of Materials, 1974
- Coupled Blade-Disk-Shroud Flutter Instabilities in Turbojet Engine RotorsJournal of Engineering for Power, 1967
- Effect of Mistuning on the Vibration of Turbo-Machine Blades Induced by WakesJournal of Mechanical Engineering Science, 1966
- System Mode Shapes in the Flutter of Compressor Blade RowsJournal of the Aeronautical Sciences, 1956