The Use of Actuator‐Disc Dynamic Inflow for Helicopter Flap‐Lag Stability
- 1 July 1983
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 28 (3), 79-88
- https://doi.org/10.4050/jahs.28.79
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- Theoretical Flap‐Lag Damping with Various Dynamic Inflow ModelsJournal of the American Helicopter Society, 1980
- Use of Multiblade Coordinates for Helicopter Flap-Lag Stability with Dynamic InflowJournal of Aircraft, 1980
- Parameter Identification Applied to Analytic Hingeless Rotor ModelingJournal of the American Helicopter Society, 1979
- High-Speed Helicopter Impulsive NoiseJournal of the American Helicopter Society, 1977
- Technical Notes: Application of Simplified Inflow Models to Rotorcraft Dynamic AnalysisJournal of the American Helicopter Society, 1976
- Model tests on unsteady rotor wake effects.Journal of Aircraft, 1973