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Comparison of industrial and scientific CFD approaches for predicting cross wind stability of the NGT2 model train geometry

Comparison of industrial and scientific CFD approaches for predicting cross wind stability of the NGT2 model train geometry
Comparison of industrial and scientific CFD approaches for predicting cross wind stability of the NGT2 model train geometry
Safety assessments of cross-wind influence on high-speed train operation require a detailed investigation of the aerodynamic forces acting on a vehicle. European norm 14067-6 permits the derivation of required integral force and moment coefficients by experiments as well as by numerical simulation. Utilizing the DLR’s Next Generation Train 2 model geometry, we have performed a case study comparing simulations with varying turbulence modeling assumptions. Because of its relevance for actual design, a focus lies on steady RANS computations, but more expensive unsteady RANS (URANS) and delayed detached eddy simulations (DDES) have also been carried out for comparison. Validation data for the exact same model configuration and moderate Reynolds numbers 250,000 and 450,000 is provided by side wind tunnel experiments. Particular emphasis is laid on simulating a yaw angle of 30º, for which a major vortex system on the leeward side of the train leads to sizeable uncertainties in predicted integral coefficients. At small to intermediate wind angles the flow remains attached and absolute errors in integral quantities decline with decreasing yaw angles. However, a consistent relative difference to the experimental results greater than 10% raises doubts about the general reliability of CFD methods, that are not capable of capturing laminar-turbulent transition, which is observed for scaled models in industry type wind tunnel experiments.
2049-5358
1-28
Fragner, M.M.
3abd27e2-df7d-4087-90cb-8fbcc0b99658
Weinman, K.A.
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Deiterding, R.
ce02244b-6651-47e3-8325-2c0a0c9c6314
Fey, U.
399e9797-eb31-431b-86e1-16080b45d45a
Wagner, C.
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Fragner, M.M.
3abd27e2-df7d-4087-90cb-8fbcc0b99658
Weinman, K.A.
dcbc2be5-2d14-4edb-9b2f-97c5b98f6cb3
Deiterding, R.
ce02244b-6651-47e3-8325-2c0a0c9c6314
Fey, U.
399e9797-eb31-431b-86e1-16080b45d45a
Wagner, C.
036cef63-87f1-4dd5-8d8a-e11c526850df

Fragner, M.M., Weinman, K.A., Deiterding, R., Fey, U. and Wagner, C. (2015) Comparison of industrial and scientific CFD approaches for predicting cross wind stability of the NGT2 model train geometry. The International Journal of Railway Technology, 4 (1), 1-28. (doi:10.4203/ijrt.4.1.1).

Record type: Article

Abstract

Safety assessments of cross-wind influence on high-speed train operation require a detailed investigation of the aerodynamic forces acting on a vehicle. European norm 14067-6 permits the derivation of required integral force and moment coefficients by experiments as well as by numerical simulation. Utilizing the DLR’s Next Generation Train 2 model geometry, we have performed a case study comparing simulations with varying turbulence modeling assumptions. Because of its relevance for actual design, a focus lies on steady RANS computations, but more expensive unsteady RANS (URANS) and delayed detached eddy simulations (DDES) have also been carried out for comparison. Validation data for the exact same model configuration and moderate Reynolds numbers 250,000 and 450,000 is provided by side wind tunnel experiments. Particular emphasis is laid on simulating a yaw angle of 30º, for which a major vortex system on the leeward side of the train leads to sizeable uncertainties in predicted integral coefficients. At small to intermediate wind angles the flow remains attached and absolute errors in integral quantities decline with decreasing yaw angles. However, a consistent relative difference to the experimental results greater than 10% raises doubts about the general reliability of CFD methods, that are not capable of capturing laminar-turbulent transition, which is observed for scaled models in industry type wind tunnel experiments.

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Accepted/In Press date: August 2015
e-pub ahead of print date: September 2015
Published date: 1 November 2015
Organisations: Aerodynamics & Flight Mechanics Group

Identifiers

Local EPrints ID: 380657
URI: http://eprints.soton.ac.uk/id/eprint/380657
ISSN: 2049-5358
PURE UUID: e4bdb5b5-a5e3-4651-a246-4d82cf91c821
ORCID for R. Deiterding: ORCID iD orcid.org/0000-0003-4776-8183

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Date deposited: 08 Sep 2015 14:29
Last modified: 15 Mar 2024 03:52

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Contributors

Author: M.M. Fragner
Author: K.A. Weinman
Author: R. Deiterding ORCID iD
Author: U. Fey
Author: C. Wagner

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