Flap-lag damping of an elastic rotor blade with torsion and dynamic inflow in hover from symbolically generated equations
- 14 May 1984
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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- Theoretical Flap‐Lag Damping with Various Dynamic Inflow ModelsJournal of the American Helicopter Society, 1980
- Non-linear flap-lag dynamics of hingeless helicopter blades in hover and in forward flightJournal of Sound and Vibration, 1973
- Linear Flap-Lag Dynamics of Hingeless Helicopter Rotor Blades in HoverJournal of the American Helicopter Society, 1972
- Derivative free analogues of the Levenberg-Marquardt and Gauss algorithms for nonlinear least squares approximationNumerische Mathematik, 1971