Dynamic-stall and structural-modeling effects on helicopter blade stability with experimental correlation
- 1 April 1994
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 32 (4) , 811-819
- https://doi.org/10.2514/3.12058
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Hingeless Rotor Aeroelastic Stability Analysis with Refined Aerodynamic ModelingJournal of the American Helicopter Society, 1991
- Investigation of Dynamic Stall Effects on Isolated Rotor Flap-Lag Stability with Experimental CorrelationJournal of the American Helicopter Society, 1991
- Stability of Hingeless Rotors in Hover Using Three‐Dimensional Unsteady AerodynamicsJournal of the American Helicopter Society, 1991
- An Experimental and Analytical Investigation of Isolated Rotor Flap‐Lag Stability in Forward FlightJournal of the American Helicopter Society, 1990
- Toward a Unified Lift Model for Use in Rotor Blade Stability AnalysesJournal of the American Helicopter Society, 1985