AN INVESTIGATION OF FLAP-LAG STABILITY OF WIND TURBINE ROTORS I N THE PRESENCE OF VELOCITY GRADIENTS AND HELICOPTER ROTORS I N FORWARD FLIGHT
- 5 May 1976
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Flap-Lag Stability of Helicopter Rotor Blades in Forward FlightJournal of the American Helicopter Society, 1975
- An Application of Floquet Theory to Prediction of Mechanical InstabilityJournal of the American Helicopter Society, 1974
- Application of the Floquet Transition Matrix to Problems of Lifting Rotor StabilityJournal of the American Helicopter Society, 1971
- On the Dynamics of Lifting Rotors with Thrust or Tilting Moment Feedback ControlsJournal of the American Helicopter Society, 1970
- The Effect of Positive Pitch-flap Coupling (Negative δ3) on Rotor Blade Motion Stability and FlappingJournal of the American Helicopter Society, 1969
- Aeroelastic Instability of Torsionally Rigid Helicopter BladesJournal of the American Helicopter Society, 1967
- Pitch‐Lag Instability of Helicopter RotorsJournal of the American Helicopter Society, 1958