Recent Developments in Rotary-wing Aeroelasticity
- 1 November 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (11), 1027-1041
- https://doi.org/10.2514/3.58887
Abstract
No abstract availableKeywords
This publication has 33 references indexed in Scilit:
- Influence of Modeling and Blade Parameters on the Aeroelastic Stability of a Cantilevered RotorAIAA Journal, 1977
- Aeroelasticity-Frontiers and BeyondJournal of Aircraft, 1976
- Aeroelastic Rotor Stability AnalysisPublished by Defense Technical Information Center (DTIC) ,1976
- Grundlagen der AeroelastikPublished by Springer Nature ,1974
- Non-linear flap-lag dynamics of hingeless helicopter blades in hover and in forward flightJournal of Sound and Vibration, 1973
- Stability of elastic bending and torsion of uniform cantilevered rotor blades in hoverPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Linear Flap-Lag Dynamics of Hingeless Helicopter Rotor Blades in HoverJournal of the American Helicopter Society, 1972
- Review of Rotary-Wing V/STOL Dynamic and Aeroelastic ProblemsJournal of the American Helicopter Society, 1969
- Pitch‐Lag Instability of Helicopter RotorsJournal of the American Helicopter Society, 1958
- Helicopter Blade Vibration and FlutterJournal of the American Helicopter Society, 1956