CCSE Home

Home

News

Research

Publications

People

AMReX

Downloads


Emmanuel Motheau

Postdoctoral Researcher, Computational Research Division


Contact Information

Emmanuel Motheau
MS 50A-3111
Lawrence Berkeley National Lab
1 Cyclotron Rd.
Berkeley, CA 94720

510-486-7286 (office)
510-486-6900 (fax)

EMotheau@lbl.gov


Affiliation and Research Interests

I am a postdoctoral researcher in the Center for Computational Sciences and Engineering (CCSE) in the Computational Research Division of the Computing Sciences Directorate at the Lawrence Berkeley National Laboratory.

My research topic is to develop a hybrid strategy to couple the fully-compressible and the low-Mach-number approaches, based on multigrids and AMR (Adaptive Mesh Refinement) methods. The challenge is to apply such strategy to combustion applications, and more specifically to the study of thermoacoustics problems and combustion instabilities.


Previous works and background

Before joining Lawrence Berkeley National Laboratory, I was a Research Associate (ARC Level B) at the University of Adelaide (Australia) and collaborated with Prof. John Abraham (Purdue University, USA). During two years (2014-2015), I have developped a DNS code named HOLOMAC (High-Order LOw MAch Combustion) to perform numerical simulations of reactive flows with detailed chemistry and under the low-Mach-number assumption.
The algorithm uses high-order numerical methods and reaches sixth-order accuracy with quasi-spectral accuracy. For detailed informations, please see Motheau and Abraham, JCP 2016. HOLOMAC is currently used in the group of Prof. John Abraham to assess petro/bio-diesel performances.

In 2013, I graduated from the Institut National Polytechnique of the University of Toulouse, France. I did my Ph.D. thesis at CERFACS (European Center for Research and Formation in Scientific Computation) under the supervision of Dr. Thierry Poinsot and Prof. Franck Nicoud. Snecma Motors (SAFRAN group) has founded the thesis. The subject of my Ph.D. thesis is the study of combustion instabilities in realistic aeronautical gas turbines, and more specifically instabilities resulting from the coupling between acoustic and entropy modes of fluctuation.

Large-Eddy Simulations (LES) were performed to reproduce stable and unstable operating points. However, despite a great agreement with the experimental results provided by the industry, LES results come at a tremendous computational cost and do not explain all the physics and why the system is unstable. An alternative approach has been developed, based on mixed numerical and analytical models. It relies on the use of a zero-Mach-number thermoacoustic Helmholtz solver together with a Delayed Entropy Coupled Boundary Condition (DECBC). Coupled with a Dynamic Mode Decomposition (DMD) analysis, such methodology is able to construct a reduced-order model so as to extract the underlying instability mechanism. The mixed acoustic-entropy nature of the mechanism has then been demonstrated. During my Ph.D. I participated in 2012 at the Summer Program of the Center for Turbulence Research, Stanford University, USA. For details, please see Motheau et al., JFM 2014 and Motheau et al., JSV 2014.

In 2010, I earned a M.Sc. in Acoustics from the Engineering School of the Conservatoire National des Arts et Metiers, Paris, France. Between 2005 and 2010, I did several internships in academic and industrial research labs: musical acoustics at the LAM (Laboratory of Musical Acoustics) in the Pierre and Marie Curie University in Paris, France; fluid-structure interactions and underwater acoustics at DCNS in Nantes, France; Large-Eddy-Simulations of multiperforated plates of gas turbine combustion chambers at Turbomeca (SAFRAN group) in Pau, France.


Refereed Journal Publications

Emmanuel Motheau, Ann Almgren, John Bell, "Navier-Stokes Characteristic Boundary Conditions Using Ghost Cells," AIAA J., Vol. 55, No. 10 : pp. 3399-3408, 2017 [pdf].

Z. Wang, E. Motheau and J. Abraham, "Effects of equivalence ratio variations on turbulent flame speed in lean methane/air mixtures under lean-burn natural gas engine operating conditions", Proc. Combust. Inst., Volume 36, Issue 3, 3423-3430, 2017. [pdf]

E. Motheau, J. Abraham, "A high-order numerical algorithm for DNS of low-Mach-number reactive flows with detailed chemistry and quasi-spectral accuracy", Journal of Computational Physics, 313, 430-454, 2016. [pdf]

E. Motheau, F. Nicoud and T. Poinsot, "Mixed acoustic-entropy combustion instabilities in gas turbines", Journal of Fluid Mechanics, 749, 542-576, 2014. [pdf]

E. Motheau, L. Selle and F. Nicoud, "Accounting for convective effects in zero-Mach-number thermoacoustic models", Journal of Sound and Vibration, 333(1), 246-262, 2014. [pdf]

E. Motheau, Y. Mery, F. Nicoud, and T. Poinsot, "Analysis and modelling of entropy modes in a realistic aeronautical gas turbine", Journal of Engineering for Gas Turbines and Power, 135(09):092602, 2013. [pdf]

E. Motheau, F. Nicoud, and T. Poinsot, "Using boundary conditions to account for mean flow effects in a zero-Mach-number acoustic solver", Journal of Engineering for Gas Turbines and Power, 134(11):111502, 2012. [pdf]

E. Motheau, T. Lederlin, Juan Florenciano, and P. Bruel, "LES investigation of the flow through an effusion-cooled aeronautical combustor model", Flow, Turbulence and Combustion, 88(March):169-189, 2012. [pdf]

Refereed Conference Proceedings

E. Motheau, A. Almgren and J.B. Bell. "Navier-Stokes Characteristic Boundary Conditions Using Ghost Cells", 23rd AIAA Computational Fluid Dynamics, Denver, CO, USA, June 6 2017. [pdf]

E. Motheau, M. Duarte, A. Almgren and J.B. Bell. " A Hybrid Adaptive Low-Mach-Number/Compressible Method for the Euler Equations", 23rd AIAA/CEAS Aeroacoustics Conference, Denver, CO, USA, June 5 2017. [pdf]

Z. Wang, E. Motheau and J. Abraham, "Equivalence Ratio Effects on Turbulent Premixed Flames in Lean Methane/Air Mixtures", Australian Combustion Symposium 2015, Melbourne (Australia), December 7-9 2015. [pdf]

E. Motheau, Y. Mery, F. Nicoud and T. Poinsot, "Analysis and modelling of entropy modes in a realistic aeronautical gas turbine", ASME Turbo Expo 2013, San Antonio (Texas, USA), June 3-7 2013, Selected for journal publication.

E. Motheau, F. Nicoud and T. Poinsot, "Using boundary conditions to account for mean flow effects in a zero-Mach-number acoustic solver", ASME Turbo Expo 2012, Copenhagen (Denmark), June 11-15 2012, Selected for journal publication.

E. Motheau, T. Lederlin, and P. Bruel, "LES investigation of the flow through an effusion-cooled aeronautical combustor model", ETMM8: 8th International ERCOFTAC Symposium, Marseille, France, June 9-11 2010, Selected for journal publication.

Peer-reviewed Conference Publications

E. Motheau, L. Selle, Y. Mery, T. Poinsot, and F. Nicoud, "A mixed acoustic-entropy combustion instability in a realistic gas turbine", Center for Turbulence Research, Proceedings of the Summer Program, Stanford University, 2012. [pdf]

Presentations

E. Motheau, A. Almgren and J.B. Bell. "Navier-Stokes Characteristic Boundary Conditions Using Ghost Cells", 23rd AIAA Computational Fluid Dynamics, Denver, CO, USA, June 6 2017.

E. Motheau, M. Duarte, A. Almgren and J.B. Bell. " A Hybrid Adaptive Low-Mach-Number/Compressible Method for the Euler Equations", 23rd AIAA/CEAS Aeroacoustics Conference, Denver, CO, USA, June 5 2017.

E. Motheau, A. Almgren and J.B. Bell. "A Hybrid Adaptive Compressible/Low-Mach-Number method", SIAM-CSE17, Atlanta, USA, February 27 2017.

E. Motheau, "Towards a Hybrid Adaptive Compressible/Low-Mach-Number method", Invited talk, BASCD 2016, Stanford University, USA, December 3 2016.

Z. Wang, E. Motheau and J. Abraham, "Equivalence Ratio Effects on Turbulent Premixed Flames in Lean Methane/Air Mixtures", Australian Combustion Symposium 2015, Melbourne (Australia), December 7-9 2015.

E. Motheau, "Using Mach-number assumptions to derive CFD methods: application to reactive flows and combustion instabilities", Invited seminar, University of New South Wales, Sydney, Australia, June 3 2015.

E. Motheau, Y. Mery, F. Nicoud and T. Poinsot, "Analysis and modelling of entropy modes in a realistic aeronautical gas turbine", ASME Turbo Expo 2013, San Antonio (Texas, USA), June 3-7 2013.

E. Motheau, F. Nicoud, and T. Poinsot, "Analysis and modelling of entropy modes in a realistic aeronautical gas turbine", Journee des Doctorants, Snecma Motors, Safran Group, Villaroche, France, May 2013.

E. Motheau, F. Nicoud and T. Poinsot, "Using boundary conditions to account for mean flow effects in a zero-Mach-number acoustic solver", ASME Turbo Expo 2012, Copenhagen (Denmark), June 11-15 2012.

E. Motheau, F. Nicoud, and T. Poinsot, "Using boundary conditions to account for mean flow effects in a zero-Mach-number acoustic solver", Journee des Doctorants, Turbomeca, Safran Group, Bordes, France, December 2011.

E. Motheau, F. Nicoud, and T. Poinsot, "Using boundary conditions to account for mean flow effects in a zero-Mach-number acoustic solver", Journee des Doctorants, Groupe Francais de Combustion, Ecole Centrale Paris, Paris, France, December 15 2011.

E. Motheau, F. Nicoud, and T. Poinsot, "Using boundary conditions to account for mean flow effects in a zero-Mach-number acoustic solver", 3rd INCA Colloquim, Toulouse, France, November 17-18 2011.

E. Motheau, T. Lederlin, and P. Bruel, "LES investigation of the flow through an effusion-cooled aeronautical combustor model", ETMM8: 8th International ERCOFTAC Symposium, Marseille, France, June 9-11 2010.

Other academic activities

Reviewing activities for Combustion Science and Technology (Taylor & Francis), Energies (MDPI), Journal of Fluids Engineering (ASME), Journal of Fluid Mechanics (Cambridge University Press), International Journal of Aeroacoustics (Multi-Science).