Coupled Flap‐Lag‐Torsional Dynamics of Hingeless Rotor Blades in Forward Flight
- 1 October 1982
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 27 (4) , 28-36
- https://doi.org/10.4050/jahs.27.28
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- 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
- Examination of the flap-lag stability of rigid articulated rotor bladesJournal of Aircraft, 1979
- Aeroelastic stability and response of horizontal axis wind turbine bladesAIAA Journal, 1979
- Recent Developments in Rotary-wing AeroelasticityJournal of Aircraft, 1977
- Efficient numerical treatment of periodic systems with application to stability problemsInternational Journal for Numerical Methods in Engineering, 1977
- Validation of Rotorcraft Flight Simulation Program through Correlation with Flight Data for Soft-in-Plane Hingeless RotorsPublished by Defense Technical Information Center (DTIC) ,1976
- Flap-Lag Stability of Helicopter Rotor Blades in Forward FlightJournal of the American Helicopter Society, 1975
- Galerkin's procedure for nonlinear periodic systemsArchive for Rational Mechanics and Analysis, 1965