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The TILDA Project—Objectives, Project and Activities Read chapter Read first chapter

2021 | OriginalPaper | Chapter

NASA Rotor 37

Authors : S. Mouriaux, F. Bassi, A. Colombo, A. Ghidoni

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

Publisher: Springer International Publishing

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Abstract

The NASA Rotor 37 is an isolated transonic axial compressor rotor. This case was initially included in a wider research program to cover a range of design parameters typical of high pressure compressor inlet stage of aircraft engines. Most numerical studies fail at predicting with accuracy the overall performance, e.g., the adiabatic efficiency and the losses distribution downstream of the blade. This case presents indeed several phenomena which are challenging to capture: laminar-to-turbulent transition on the blade, interaction of the boundary layer with the shock, secondary and tip-leakage flows. If LES appears a more adequate tool than RANS to predict such inherently unsteady phenomena, it remains delicate, especially because wall modeling is required. This section presents results obtained by Safran and UniBG of WMLES using the Discontinuous Galerkin approach.

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previous chapter Detached-Eddy Simulation of Dual Stream Nozzle Jet Using High Order Discontinuous Galerkin Method
next chapter Conclusion and Prospects
Literature
1.
F. Bassi, L. Botti, A. Colombo, A. Crivellini, C. De Bartolo, N. Franchina, A. Ghidoni, S. Rebay, Time integration in the discontinuous Galerkin code MIGALE: steady problems, in IDIHOM: Industrialization of High-Order Methods—A Top-Down Approach. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol. 128, ed. by N. Kroll, C. Hirsch, F. Bassi, C. Johnston, K. Hillewaert (Springer International Publishing, 2015), pp. 179–204
2.
F. Bassi, L. Botti, A. Colombo, A. Crivellini, A. Ghidoni, A. Nigro, S. Rebay. Time integration in the discontinuous Galerkin code MIGALE: unsteady problems, in IDIHOM: Industrialization of High-Order Methods—A Top-Down Approach, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol. 128, ed. by N. Kroll, C. Hirsch, F. Bassi, C. Johnston, K. Hillewaert (Springer International Publishing, 2015), pp. 205–230
3.
F. Bassi, L. Botti, A. Colombo, D.A. Di Pietro, P. Tesini. On the flexibility of agglomeration based physical space discontinuous Galerkin discretizations. J. Comput. Phys. 45–65 (2012)
4.
F. Bassi, L. Botti, A. Colombo, A. Ghidoni, F. Massa, G. Noventa, On the development of an implicit high-order discontinuous Galerkin solver for a hybrid RANS-LES model, in Direct and Large-Eddy Simulation XI, ed. by M. Vittoria Salvetti, V. Armenio, J. Fröhlich, B.J. Geurts, H. Kuerten (Springer International Publishing, 2019), pp. 75–82
5.
F. Bassi, S. Rebay, A high-order accurate discontinuous finite element method for the numerical solution of the compressible Navier–Stokes equations. J. Comput. Phys. 131, 267–279 (1997)MathSciNetCrossRef
6.
F. Bassi, L. Botti, A. Colombo, A. Ghidoni, F. Massa, Linearly implicit Rosenbrock-type Runge–Kutta schemes applied to the Discontinuous Galerkin solution of compressible and incompressible unsteady flows. Comput. Fluids 118, 305–320 (2015)MathSciNetCrossRef
7.
F. Bassi, L. Botti, A. Colombo, A. Crivellini, N. Franchina, A. Ghidoni, Assessment of a high-order accurate discontinuous Galerkin method for turbomachinery flows. Int. J. Comput. Fluid Dyn. 30(4), 307–328 (2016)MathSciNetCrossRef
8.
9.
J. Dunham, CFD validation for propulsion system components (la validation CFD des organes des propulseurs) (Technical report, Advisory Group for Aerospace Research and Development Neuilly-Sur-Seine (FRANCE), 1998)
10.
J. Dunham. CFD validation for propulsion system components. Technical Report AR-355, AGARD, 1994
11.
A. Frère, C.C. de Wiart, K. Hillewaert, P. Chatelain, G. Winckelmans, Application of wall-models to discontinuous Galerkin les. Phys. Fluids 29(8), 085111 (2017)
12.
C. Geuzaine, J.F. Remacle, Gmsh: A 3-D finite element mesh generator with built-in-pre-and post-processing facilities. Int. J. Num. Method. Eng. 79(11), 1309–1331 (2009)
13.
A. Gomar, N. Gourdain, G. Dufour. High fidelity simulation of the turbulent flow in a transonic axial compressor (2011)
14.
D. Hänel, R. Schwane, G. Seider. On the accuracy of upwind schemes for the solution of the Navier–Stokes equations. AIAA Paper 87-1105 (1987)
15.
K. Hillewaert, Development of the Discontinuous Galerkin Method for High-Resolution, Large Scale CFD and Acoustics in Industrial Geometries (Presses univ. de Louvain, 2013)
16.
J. Joo, G. Medic, D.A. Philips, S. Bose, Large-eddy simulation of a compressor rotor, in Proceedings of the Summer Program (2014), p. 467
17.
J.C. Kok, H.S. Dol, B. Oskam, H. van der Ven, Extra-large eddy simulation of massively separated flows, in 42nd AIAA Aerospace Sciences Meeting and Exhibit (2004)
18.
J. Lang, J. Verwer, ROS3P-An accurate third-order Rosenbrock solver designed for parabolic problems. BIT Numer. Math. 41(4), 731–738 (2001)
19.
D. Moxey, D. Ekelschot, Ü. Keskin, S.J. Sherwin, J. Peiró, A thermo-elastic analogy for high-order curvilinear meshing with control of mesh validity and quality. Proced. Eng. 82, 127–135 (2014)CrossRef
20.
D. Papadogiannis, X. Garnaud, Unstructured large eddy simulations of the transonic compressor rotor 37, in 23rd AIAA Computational Fluid Dynamics Conference (2017), p. 3612
21.
P. Persson, J. Peraire, Curved mesh generation and mesh refinement using Lagrangian solid mechanics, in 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition (2009), p. 949
22.
P. Persson, J. Peraire, Sub-cell shock capturing for discontinuous Galerkin methods, in 44th AIAA Aerospace Sciences Meeting and Exhibit (2006), p. 112
23.
F. Renac, M. de la Llave Plata, E. Martin, J.B. Chapelier, V. Couaillier, Aghora: a high-order DG solver for turbulent flow simulations, in IDIHOM: Industrialization of High-Order Methods—A Top-Down Approach: Results of a Collaborative Research Project Funded by the European Union, 2010–2014, ed. by N. Kroll, C. Hirsch, F. Bassi, C. Johnston, K. Hillewaert (Springer International Publishing, 2015), pp. 315–335
24.
A. Yoshizawa, K. Horiuti, A statistically-derived subgrid-scale kinetic energy model for the large-eddy simulation of turbulent flows. J. Phys. Soc. Jpn. 54(8), 2834–2839 (1985)CrossRef
Metadata
Title
NASA Rotor 37
Authors
S. Mouriaux
F. Bassi
A. Colombo
A. Ghidoni
Copyright Year
2021
Book
TILDA: Towards Industrial LES/DNS in Aeronautics

Print ISBN: 978-3-030-62047-9

Electronic ISBN: 978-3-030-62048-6

Copyright Year: 2021

DOI
https://doi.org/10.1007/978-3-030-62048-6_20

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