Optimal placement of tuning masses for vibration reduction in helicopter rotor blades
- 1 February 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (2), 309-315
- https://doi.org/10.2514/3.10390
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Synthesis of Dynamic Vibration AbsorbersJournal of Vibration and Acoustics, 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
- Simplified calculation of eigenvector derivativesAIAA Journal, 1976
- Some Approximation Concepts for Structural SynthesisAIAA Journal, 1974
- Effect of Spanwise and Chordwise Mass Distribution on Rotor Blade Cyclic StressesJournal of the American Helicopter Society, 1956