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2021 | OriginalPaper | Chapter

Boeing Rudimentary Landing Gear Configuration

Authors : R. Hartmann, F. Bassi, A. Colombo, A. Crivellini, M. Franciolini, F. Massa

Published in: TILDA: Towards Industrial LES/DNS in Aeronautics

Publisher: Springer International Publishing

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Abstract

This chapter includes computational details and results obtained in the EU-project TILDA on the Boeing Rudimentary Landing Gear.

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Literature
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go back to reference S.H. Peng, M. Strelets, Test Case ST12 Boeing Rudimentary Landing Gear (ATAAC, 2012) S.H. Peng, M. Strelets, Test Case ST12 Boeing Rudimentary Landing Gear (ATAAC, 2012)
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go back to reference R. Hartmann, Wall-resolved and wall-modeled ILES based on high-order DG, in Proceedings of the ECCOMAS (ECCM 6/ECFD 7) Congress 2018, Glasgow, UK, 11–15 June 2018 (2018) R. Hartmann, Wall-resolved and wall-modeled ILES based on high-order DG, in Proceedings of the ECCOMAS (ECCM 6/ECFD 7) Congress 2018, Glasgow, UK, 11–15 June 2018 (2018)
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go back to reference A. Probst, J. Löwe, S. Reuß, T. Knopp, R. Kessler, Scale-resolving simulations with a low-dissipation low-dispersion second-order scheme for unstructured flow solvers. AIAA J. 54(10), 2972–2987 (2016)CrossRef A. Probst, J. Löwe, S. Reuß, T. Knopp, R. Kessler, Scale-resolving simulations with a low-dissipation low-dispersion second-order scheme for unstructured flow solvers. AIAA J. 54(10), 2972–2987 (2016)CrossRef
Metadata
Title
Boeing Rudimentary Landing Gear Configuration
Authors
R. Hartmann
F. Bassi
A. Colombo
A. Crivellini
M. Franciolini
F. Massa
Copyright Year
2021
DOI
https://doi.org/10.1007/978-3-030-62048-6_14

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