Simulation and design analyses of turbulent combustion in Diesel engines. Prof. Dr. İ. Bedii Özdemir ITU Fluids Group & AIY Technologies

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Simulation and design analyses of turbulent combustion in Diesel engines Prof. Dr. İ. Bedii Özdemir ITU Fluids Group & AIY Technologies

Summary Stringent legislation of EURO standards on emissions from diesel engines present a strong challenge to the engine designers who are forced to produce first prototypes with a design closer to that of the final engine. Hence it becomes crucially important to develop effective numerical tools. A numerical procedure is described here with the objective of quantifying the generation and depletion of the pollutants, NO x and particulate matter emission from diesel engines. The diesel fuel reaction mechanism included 43 species and 393 reactions. The ignition was treated as a homogeneous reaction and, for the combustion at later stages, the mechanism was reduced with Intrinsic Low Dimensional Manifolds (ILDM) technique. Balance equations are solved on a moving mesh with models of spray break-up and evaporation. The turbulence-chemistry reciprocity was based on the concept of the time-layered ILDM. This model required a time scale from a 3-D turbulent reacting flow, and is able to retrieve the corresponding local mean source values from a pre-processed data base. The main advantage of this method is to take into account nonequilibrium states of the combustion thermo-chemistry.

Introduction With the advance of combustion technologies, use of Diesel engines rapidly spreads from its conventional use in heavy duty applications to light vehicles. Stringent regulations on the emissions of NO x and soot, however, force the manufacturers to re-design the Diesel incylinder processes. Efforts along these directions have eventually led to new concepts, as for example, high swirl in-cylinder flows, high pressure injections, etc. Complex designs require complex models which are difficult to adapt to a wider ranges of design parameters. Attempts for 3D simulation with global chemistry cannot capture the details of auto-ignition process and suffer from the lack of intermediate species, which proves to be very important for emission predictions. It appears that better modelling of turbulent mixing with reduced chemistry improves significantly the accuracy of the simulations. An important approach to trace chemistry of pollutant formation is to use Intrinsic Low Dimensional Manifolds (ILDM) technique as a reduction scheme. The key issue in turbulent combustion is to model turbulence-chemistry reciprocity: Transport of joint pdf models produces most accurate results but it is computationally expensive and nearly impossible to use in engine geometries. Therefore, presumed pdf methods are widely used in engineering calculations.

ILDM Chemistry Figure 1. Fast reactions are relaxed to manifold of slow reactions [U. Maas and S. B. Pope (1992)]. From the system dynamics perspective, a chemical process with n s species will be governed by n s different time scales. ILDM, in principle, tries to find out the directions in which the chemical source term vector will rapidly reach a steady-state. If n f fast processes are assumed in dynamic equilibrium, the system can be described by n r = n s - n f degrees of freedom by mixture fraction, pressure, enthalpy and n r progress variables which parameterize the slow movement on the manifold. This reduces the chemical system in the composition space and the number of transport equations that need to be solved and, also, reduces the dimension of the probability density function that the reaction rate needs to be integrated over in turbulent flows.

Governing Equations ALU (Arbitrary Lagrangian Eulerian) method is used to solve the equations expressing conservation of mixture mass, momentum, enthalpy expressed as, where s refers spray and c chemistry-related terms. The equation for the mean mixture fraction, is solved together with the equation for its variance. For reaction progress variables, as for example CO 2, the transport is given as, and its variance where averaged quantities are defined using, and

CFD Implementation; An application Injection velocity [cm/s] The computational setup is designed to match FORD I5, a 5-cylinder diesel engine with 3.2 lt cylinder volume, which was disretized in 174176 cells as shown in Figure 2, Figure 2. Computational domain. The spray injection profile is shown in Figure 3. Crank angle [degrees] Figure 3. Injection timing.

Results; Mixture fraction 354 KA 354 KA 371 KA 355 KA 364 KA 372 KA 356 KA 366 KA 375 KA 359 KA 367 KA 377 KA 362 KA 369 KA 379 KA 363 KA 370 KA 382 KA

Results; Temperature 354 KA 354 CA 371 CA 355 CA 364 CA 372 CA 356 CA 366 CA 375 CA 359 CA 367 CA 377 CA 362 CA 369 CA 379 CA 363 CA 370 CA 382 CA

Results; CO 2 Mass fraction 354 KA 354 KA 371 KA 355 KA 364 KA 372 KA 356 KA 366 KA 375 KA 359 KA 367 KA 377 KA 362 KA 369 KA 379 KA 363 KA 370 KA 382 KA

Results; H 2 O Mass fraction 354 KA 354 KA 371 KA 355 KA 364 KA 372 KA 356 KA 366 KA 375 KA 359 KA 367 KA 377 KA 362 KA 369 KA 379 KA 363 KA 370 KA 382 KA

Results; NO Mass fraction 354 KA 354 KA 371 KA 355 KA 364 KA 372 KA 356 KA 366 KA 375 KA 359 KA 367 KA 377 KA 362 KA 369 KA 379 KA 363 KA 370 KA 382 KA

Results; CO Mass fraction 354 KA 354 KA 371 KA 355 KA 364 KA 372 KA 356 KA 366 KA 375 KA 359 KA 367 KA 377 KA 362 KA 369 KA 379 KA 363 KA 370 KA 382 KA

Results; Soot precursor & soot volume fraction 354 KA 354 KA 371 KA 354 KA 354 KA 371 KA 355 KA 364 KA 372 KA 355 KA 364 KA 372 KA 356 KA 366 KA 375 KA 356 KA 366 KA 375 KA 359 KA 367 KA 377 KA 359 KA 367 KA 377 KA 362 KA 369 KA 379 KA 362 KA 369 KA 379 KA 363 KA 370 KA 382 KA 363 KA 370 KA 382 KA

Results; Soot vs crank angle N s [1/cm 3 ] Crank Angle [degree]