Flap‐Lag‐Torsion Stability in Forward Flight
- 1 October 1985
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 30 (4) , 30-39
- https://doi.org/10.4050/jahs.30.30
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- The Use of Actuator‐Disc Dynamic Inflow for Helicopter Flap‐Lag StabilityJournal of the American Helicopter Society, 1983
- Some analysis methods for rotating systems with periodic coefficientsAIAA Journal, 1983
- Improved Methods in Ground Vibration TestingJournal of the American Helicopter Society, 1983
- Coupled Flap‐Lag‐Torsional Dynamics of Hingeless Rotor Blades in Forward FlightJournal of the American Helicopter Society, 1982
- Theoretical Flap‐Lag Damping with Various Dynamic Inflow ModelsJournal of the American Helicopter Society, 1980
- Examination of the flap-lag stability of rigid articulated rotor bladesJournal of Aircraft, 1979
- Recent Developments in Rotary-wing AeroelasticityJournal of Aircraft, 1977
- Flap-Lag Stability of Helicopter Rotor Blades in Forward FlightJournal of the American Helicopter Society, 1975
- Some Approximations to the Flapping Stability of Helicopter RotorsJournal of the American Helicopter Society, 1974
- Linear Flap-Lag Dynamics of Hingeless Helicopter Rotor Blades in HoverJournal of the American Helicopter Society, 1972