Unsteady wake effects on progressing/regressing forced rotor flapping modes
- 16 August 1972
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- The Wake Geometry of a Hovering Helicopter Rotor and Its Influence on Rotor PerformanceJournal of the American Helicopter Society, 1972
- Articulated Rotor Blade Flapping Motion at Low Advance RatioJournal of the American Helicopter Society, 1972
- On the Computation of Airloads Acting on Rotor Blades in Forward FlightJournal of the American Helicopter Society, 1962
- Investigation of Helicopter Blade Flutter and Load Amplification ProblemsJournal of the American Helicopter Society, 1957