Model tests on unsteady rotor wake effects.
- 1 January 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 10 (1), 58-60
- https://doi.org/10.2514/3.44350
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Hingeless Helicopter Rotor Response with Nonuniform Inflow and Elastic Blade BendingJournal of Aircraft, 1972
- Unsteady rotor aerodynamics at low inflow and its effect on flutterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Unsteady wake effects on progressing/regressing forced rotor flapping modesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Some Applications of the Method of Multiblade CoordinatesJournal of the American Helicopter Society, 1972