Aeroelastic tailoring of rotor blades for vibration reduction in forward flight
- 2 May 1983
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Coupled Flap‐Lag‐Torsional Dynamics of Hingeless Rotor Blades in Forward FlightJournal of the American Helicopter Society, 1982
- On Making Things the Best-Aeronautical Uses of OptimizationJournal of Aircraft, 1982
- Application of the Finite Element Method to Rotary‐Wing AeroelasticityJournal of the American Helicopter Society, 1980
- Second order approximation of natural frequency constraints in structural synthesisInternational Journal for Numerical Methods in Engineering, 1978
- Recent Developments in Rotary-wing AeroelasticityJournal of Aircraft, 1977
- Techniques for stability analysis and design optimization with dynamic constraints of nonconservative linear systemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Helicopter Blade Vibration and FlutterJournal of the American Helicopter Society, 1956
- Effect of Spanwise and Chordwise Mass Distribution on Rotor Blade Cyclic StressesJournal of the American Helicopter Society, 1956