Effect of Steady State Coning Angle and Damping on Whirl Flutter Stability
- 1 November 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 10 (11) , 664-669
- https://doi.org/10.2514/3.60280
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Principles of Structural StabilityPublished by Springer Nature ,1977
- Review of rotary-wing V/STOL dynamic and aeroelastic problemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- The Influence of Blade Flapping Restraint on the Dynamic Stability of Low Disk Loading Propeller‐RotorsJournal of the American Helicopter Society, 1967
- Propeller-rotor whirl flutter: A state-of-the-art reviewJournal of Sound and Vibration, 1966