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.
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
May 2017
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, .
(doi:10.1016/j.jfluidstructs.2017.03.004).
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.
Text
Gust load analysis using computational fluid dynamics derived reduced order models
- Accepted Manuscript
More information
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
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Date deposited: 09 Jun 2017 09:40
Last modified: 16 Mar 2024 05:10
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Author:
S. Timme
Author:
K.J. Badcock
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