Modeling issues related to vibration prediction of a coupled rotor/fuselage system
- 7 April 1997
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- ACSR system for vibration suppression in coupled helicopter rotor/flexible fuselage modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- A coupled helicopter rotor/fuselage aeroelastic response model for ACSRPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- EFFECT OF MODELING TECHNIQUES IN THE COUPLED ROTOR-BODY VIBRATION ANALYSISPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Validation of approximate indicial aerodynamic functions for two-dimensional subsonic flowJournal of Aircraft, 1988
- Helicopter Vibrations: A Technological PerspectiveJournal of the American Helicopter Society, 1984