Optimal placement of tuning masses for vibration reduction in helicopter rotor blades
- 18 April 1988
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Structural optimization with dynamic behavior constraintsAIAA Journal, 1985
- Optimal frequency response shaping by appendant structuresJournal of Sound and Vibration, 1984
- Blade Design for Reduced Helicopter VibrationJournal of the American Helicopter Society, 1983
- Structural optimization by multilevel decompositionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- SYSTEMATIC CONTROL DESIGN BY OPTIMIZING A VECTOR PERFORMANCE INDEXPublished by Elsevier ,1980
- Systematic Control Design by Optimizing a Vector Performance IndexIFAC Proceedings Volumes, 1979
- Modal Analysis of Rotating Flexible StructuresAIAA Journal, 1976
- Simplified calculation of eigenvector derivativesAIAA Journal, 1976
- Some Approximation Concepts for Structural SynthesisAIAA Journal, 1974
- Rates of change of eigenvalues and eigenvectors.AIAA Journal, 1968