A coupled helicopter rotor/fuselage aeroelastic response model for ACSR
- 10 April 1995
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Correlation studies for hingeless rotors in forward flightPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Aeroelastic response and blade loads of a composite rotor in forwardflightPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Vibration reduction in helicopter rotors using an active control surface located on the bladePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- A Study of Fundamental Issues in Higher Harmonic Control Using Aeroelastic SimulationJournal of the American Helicopter Society, 1991
- Rotary-wing aeroelasticity with application to VTOL vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Higher Harmonic Control: Wind Tunnel Demonstration of Fully Effective Vibratory Hub Force SuppressionJournal of the American Helicopter Society, 1989
- Helicopter Vibrations: A Technological PerspectiveJournal of the American Helicopter Society, 1984
- Helicopter Vibration Suppression Using Simple Pendulum Absorbers on the Rotor BladeJournal of the American Helicopter Society, 1984
- Analytical and Experimental Investigation of a Bearingless Hub-AbsorberJournal of the American Helicopter Society, 1983
- Consistent mass matrices for three dimensional beam element due to distributed and lumped non-structural mass systems acting on its spanComputers & Structures, 1981