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Verification of a low fidelity fast simulation framework through RANS simulations

Carrizales, Martin A.; Dussart, Gaétan; Portapas, Vilius; Pontillo, Alessandro; Lone, Mudassir

Authors

Martin A. Carrizales

Gaétan Dussart

Alessandro Pontillo

Mudassir Lone



Abstract

© 2019, The Author(s). Verification and validation of simulation models are critical steps in engineering. This paper aims at verifying the suitability of reduced order aerodynamic models used in an aeroservoelastic framework designed to analyze the flight dynamics of flexible aircraft, known as the Cranfield Accelerated Aircraft Loads Model. This framework is designed for rapid assessment of aircraft configurations at the conceptual design stage. Therefore, it utilizes or relies on methods that are of relatively low fidelity for high computational speeds, such as modified strip theory coupled with Leishmann–Beddoes unsteady aerodynamic model. Hence, verification against higher order methods is required. Although low fidelity models are widely used for conceptual design and loads assessments, the open literature still lacks a comparison against higher fidelity models. This work focuses on steady-trimmed flight conditions and investigates the effect of aerodynamic wing deformation under such loads on aerodynamic performance. Key limitations of the reduced order models used, namely fuselage and interference effects, are discussed. The reasons for the overall agreement between the two approaches are also outlined.

Citation

Carrizales, M. A., Dussart, G., Portapas, V., Pontillo, A., & Lone, M. (2020). Verification of a low fidelity fast simulation framework through RANS simulations. CEAS Aeronautical Journal, 11(1), 161-176. https://doi.org/10.1007/s13272-019-00409-x

Journal Article Type Article
Acceptance Date Jul 4, 2019
Online Publication Date Jul 22, 2019
Publication Date Jan 1, 2020
Deposit Date Jan 28, 2020
Journal CEAS Aeronautical Journal
Print ISSN 1869-5582
Electronic ISSN 1869-5590
Publisher Springer (part of Springer Nature)
Peer Reviewed Peer Reviewed
Volume 11
Issue 1
Pages 161-176
DOI https://doi.org/10.1007/s13272-019-00409-x
Keywords Aerospace Engineering; Transportation
Public URL https://uwe-repository.worktribe.com/output/5260261
Publisher URL https://link.springer.com/content/pdf/10.1007/s13272-019-00409-x.pdf
Additional Information Received: 17 April 2018; Revised: 9 April 2019; Accepted: 4 July 2019; First Online: 22 July 2019

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Verification of a low fidelity fast simulation framework through RANS simulations (3 Mb)
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Licence
http://creativecommons.org/licenses/by/4.0/

Publisher Licence URL
http://creativecommons.org/licenses/by/4.0/

Copyright Statement
Open Access This article is distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativeco
mmons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.







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