The Effect of Positive Pitch-flap Coupling (Negative δ3) on Rotor Blade Motion Stability and Flapping
- 1 April 1969
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 14 (2) , 49-67
- https://doi.org/10.4050/jahs.14.49
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Tilt Proprotor Composite Aircraft, Design State of the ArtJournal of the American Helicopter Society, 1969
- The Influence of Blade Flapping Restraint on the Dynamic Stability of Low Disk Loading Propeller‐RotorsJournal of the American Helicopter Society, 1967
- 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
- Analysis of the Vertical Flight Dynamic Characteristics of the Lifting Rotor with Floating Hub and Off‐Set Coning HingesJournal of the American Helicopter Society, 1958
- Pitch‐Lag Instability of Helicopter RotorsJournal of the American Helicopter Society, 1958