Efficient numerical methods for aeroelastic analysis of wing-propeller configuration compound helicopters
Presentation / Conference
Efficient numerical methods for time-domain aeroelastic analysis of a wing structure under a propeller-wing configuration is described in the paper. A linear beam model with deformable elastic axis under torsion and flapping is considered to simulate... Read More about Efficient numerical methods for aeroelastic analysis of wing-propeller configuration compound helicopters.