Analysis of axisymmetric body effects on rotor aerodynamics using modified slender body theory
- 17 August 1984
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Reduction of Helicopter Vibration Through Control of Hub-ImpedanceJournal of the American Helicopter Society, 1980
- Interactional Aerodynamics—A New Challenge to Helicopter TechnologyJournal of the American Helicopter Society, 1980
- Aeroelastic Characteristics of Composite Bearingless Rotor BladesJournal of the American Helicopter Society, 1977
- Aerodynamic Technology for Advanced Rotorcraft—Part IIJournal of the American Helicopter Society, 1977