Structural optimization with aeroelastic constraints of rotor bladeswith straight and swept tips
- 1 May 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (5) , 928-936
- https://doi.org/10.2514/3.25141
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Rotor blade aeroelasticity in forward flight with an implicit aerodynamic formulationAIAA Journal, 1988
- Application of Design Optimization Techniques to Rotor Dynamics ProblemsJournal of the American Helicopter Society, 1988
- Aeroelastic Modeling of Swept Tip Rotor Blades Using Finite ElementsJournal of the American Helicopter Society, 1988
- Design sensitivity analysis for an aeroelastic optimization of a helicopter bladePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Design of helicopter rotor blades for optimum dynamic characteristicsComputers & Mathematics with Applications, 1986
- Optimum Design of Rotor Blades for vibration Reduction in Forward FlightJournal of the American Helicopter Society, 1984
- Aeroelastic tailoring of rotor blades for vibration reduction in forward flightPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Coupled Flap‐Lag‐Torsional Dynamics of Hingeless Rotor Blades in Forward FlightJournal of the American Helicopter Society, 1982
- Structural synthesis - Its genesis and developmentAIAA Journal, 1981
- Structural optimization by methods of feasible directionsComputers & Structures, 1973