Computationally-efficient aeroelastic analysis tool for short-wing/propeller configuration on compound helicopters

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Computationally-efficient aeroelastic analysis tool for short-wing/propeller configuration on compound helicopters

A time-domain aeroelastic analysis for short-wing/propeller configuration in compound helicopters is presented in this paper. A linear Timoshenko beam is used in conjunction with analytical aerodynamic theories, while propeller effects are simplified as defined velocity profiles in the advancing and...

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Bibliographic Details
Main Authors:	Wang, Zi, Popov, Atanas A.
Format:	Conference or Workshop Item
Language:	English
Published:	2018
Online Access:	https://eprints.nottingham.ac.uk/55088/

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