Time-domain aeroelastic model for compound helicopter propeller-wing configuration

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Time-domain aeroelastic model for compound helicopter propeller-wing configuration

A simplified numerical model for time-domain aeroelastic analysis of a wing structure in a propeller-wing configuration is described in the paper. A linear beam model with deformable elastic axis under torsional deformation and out-of-plane bending is considered to simulate a wing structure with tip...

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Bibliographic Details
Main Authors:	Wang, Zi, Anobile, Alessandro, Popov, Atanas A.
Format:	Conference or Workshop Item
Published:	2017
Subjects:	Aeroelasticity Rotorcraft Compound helicopter Wing-propeller interaction
Online Access:	https://eprints.nottingham.ac.uk/53163/

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