Efficient numerical methods for aeroelastic analysis of wing-propeller configuration compound helicopters

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Efficient numerical methods for aeroelastic analysis of wing-propeller configuration compound helicopters

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 a wing structure with a tipmounted propeller, rel...

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Bibliographic Details
Main Authors:	Wang, Zi, Anobile, Alessandro, Popov, Atanas A.
Format:	Conference or Workshop Item
Published:	2017
Subjects:	Aeroelasticity Compound helicopter Numerical method
Online Access:	https://eprints.nottingham.ac.uk/53162/

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