Linear Flap-Lag Dynamics of Hingeless Helicopter Rotor Blades in Hover
- 1 April 1972
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 17 (2), 2-14
- https://doi.org/10.4050/jahs.17.2
Abstract
No abstract availableThis publication has 3 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
- Aeroelastic Instability of Torsionally Rigid Helicopter BladesJournal of the American Helicopter Society, 1967
- A Theory of Rotor Blade Motion Stability in Powered FlightJournal of the American Helicopter Society, 1964