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Gust load analysis using computational fluid dynamics derived reduced order models

Gust load analysis using computational fluid dynamics derived reduced order models
Gust load analysis using computational fluid dynamics derived reduced order models
Time domain gust response analysis based on large order nonlinear aeroelastic models is computationally expensive. An approach to the reduction of nonlinear models for gust response prediction is presented in this paper. The method uses information on the eigenspectrum of the coupled system Jacobian matrix and projects the full order model, through a series expansion, onto a small basis of eigenvectors which is capable of representing the full order model dynamics. The novelty in the paper concerns the representation of the gust term in the reduced model in a manner consistent with standard synthetic gust definitions, allowing a systematic investigation of the influence of a large number of gust shapes without regenerating the reduced model. Results are presented for the Goland wing/store configuration.
0889-9746
116-125
Timme, S.
d688c7f1-3a3d-44e0-ad8c-15f350c91ff8
Badcock, K.J.
f7ae5be8-8140-4e46-81f8-8d1021fd989f
Da Ronch, A.
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Timme, S.
d688c7f1-3a3d-44e0-ad8c-15f350c91ff8
Badcock, K.J.
f7ae5be8-8140-4e46-81f8-8d1021fd989f
Da Ronch, A.
a2f36b97-b881-44e9-8a78-dd76fdf82f1a

Timme, S., Badcock, K.J. and Da Ronch, A. (2017) Gust load analysis using computational fluid dynamics derived reduced order models. Journal of Fluids and Structures, 71, 116-125. (doi:10.1016/j.jfluidstructs.2017.03.004).

Record type: Article

Abstract

Time domain gust response analysis based on large order nonlinear aeroelastic models is computationally expensive. An approach to the reduction of nonlinear models for gust response prediction is presented in this paper. The method uses information on the eigenspectrum of the coupled system Jacobian matrix and projects the full order model, through a series expansion, onto a small basis of eigenvectors which is capable of representing the full order model dynamics. The novelty in the paper concerns the representation of the gust term in the reduced model in a manner consistent with standard synthetic gust definitions, allowing a systematic investigation of the influence of a large number of gust shapes without regenerating the reduced model. Results are presented for the Goland wing/store configuration.

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Gust load analysis using computational fluid dynamics derived reduced order models - Accepted Manuscript
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Accepted/In Press date: 16 March 2017
e-pub ahead of print date: 13 April 2017
Published date: May 2017
Organisations: Aerodynamics & Flight Mechanics Group

Identifiers

Local EPrints ID: 410803
URI: http://eprints.soton.ac.uk/id/eprint/410803
ISSN: 0889-9746
PURE UUID: f7cc265d-e59a-4123-9b0f-bdfaede9ba7d
ORCID for A. Da Ronch: ORCID iD orcid.org/0000-0001-7428-6935

Catalogue record

Date deposited: 09 Jun 2017 09:40
Last modified: 16 Mar 2024 05:10

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Contributors

Author: S. Timme
Author: K.J. Badcock
Author: A. Da Ronch ORCID iD

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