On the Dynamics of Lifting Rotors with Thrust or Tilting Moment Feedback Controls
- 1 January 1970
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 15 (1) , 42-54
- https://doi.org/10.4050/jahs.15.42
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- The Effect of Positive Pitch-flap Coupling (Negative δ3) on Rotor Blade Motion Stability and FlappingJournal of the American Helicopter Society, 1969
- Methods for Improving Flying Qualities of Compound AircraftJournal of the American Helicopter Society, 1968
- Response Characteristics of the Gyro‐Controlled Lockheed Rotor SystemJournal of the American Helicopter Society, 1967
- Aeroelastic Instability of Torsionally Rigid Helicopter BladesJournal of the American Helicopter Society, 1967
- A Type of Lifting Rotor with Inherent StabilityJournal of the Aeronautical Sciences, 1950