Direct Numerical Simulation of Autoignition in a Jet in a Cross-Flow ...

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Contents1 Introduction 11.1 Overview of the Numerical Method . . . . . . . . . . . . . . . . 11.1.1 Summary of Numerical Simulations . . . . . . . . . . . . 32 Parallel Scaling and parallel efficiency metrics 42.1 Measurement of Parallel Efficiency . . . . . . . . . . . . . . . . . 42.1.1 Core-level MPI Threading Efficiency . . . . . . . . . . . 42.1.2 Strong Scaling Experiment . . . . . . . . . . . . . . . . . 52.2 Profiling and Hardware Performance Monitoring . . . . . . . . . 52.2.1 IBM HPC Toolkit . . . . . . . . . . . . . . . . . . . . . . 62.2.2 Nek5000 Instrumentation . . . . . . . . . . . . . . . . . . 72.2.3 Sample MPI Profile . . . . . . . . . . . . . . . . . . . . . 72.2.4 Hardware Performance . . . . . . . . . . . . . . . . . . . 83 Discussion of ESP Experience 10Bibliography 11i
Chapter 1IntroductionUnderstanding the conditions under which autoignition of reacting mixtures occursis of primary importance for the design and operation of modern lean premixed(LP) and lean premixed prevaporized (LPP) combustion devices such as low-NO xstationary gas turbines (Dobbeling et al., 2007) and propulsion devices such as subsonicramjets and supersonic scramjets (Micka and Driscoll, 2012). In particular,the enhanced turbulent mixing between the fuel and oxidizer streams of the jet incross-flow (JICF) configuration makes it an essential component in the design ofpremixing sections of modern high efficiency, low NO x combustors.The main objective of this study is to investigate the sensitivity of the JICF dynamicsto the cross-flow temperature. In particular we ask the following questions:When and where do localized flame kernels form? Could the observed ignitiontime be correlated to ignition-delay time in the corresponding homogeneous system?Do these kernels develop into stable flame later on? How does the mixtureget prepared for ignition and what is the role of the vorticity and pressure in mixingthe jet (fuel) with the cross-flow (oxidizer) fluid? What is the local combustionmode associated with the observed ignition scenarios?1.1 Overview of the Numerical MethodA weak formulation of the compressible reactive Navier-Stokes for ideal gas mixturesat the low Mach number limit were solved, using a parallel spectral-elementcode based on NEK5000 (Fischer et al., 2008). The spectral element methodis a high-order weighted residual technique that couples the rapid convergenceof global spectral methods with the geometric flexibility of finite element methods(Deville et al., 2002).A high-order operator splitting technique is used to split the thermochemistry(species and energy equations) from the hydrodynamic subsystem (continuity andmomentum equations) (Tomboulides et al., 1997). The latter is integrated in timeusing a 3rd-order semi-implicit method, with explicit treatment of the nonlinearterms and implicit treatment of the viscous and pressure terms, while the thermo-1
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