Development of a high-order discontinuous galerkin solver for internal combustion engine flows
Creato da
Covello, Vanessa
Pagnotta, Leonardo
Florio, Gaetano
De Bartolo, Carmine
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Dottorato di ricerca in Ingegneria Meccanica, XXVII Ciclo, a.a. 2014; The aim of this work is to contribute to the development of an unstructured
ow solver able to match the increasing demand of the automotive industrial
sector to advance CFD-aided design and analysis procedure. The method here
presented is designed to ensure high-order of accuracy even in complex geometries
using both explicit and implicit schemes for the temporal discretization
of the compressible Reynolds Averaged Navier-Stokes (RANS) k-omega equations.
The algorithm is based on the Discontinuous Galerkin (DG) nite element
method, one of the most promising high-order methods, that combines
excellent dispersion and dissipation properties with high geometrical
exibility.
The DG solver is based on di erent multi-stage explicit or many implicit
or semi-implicit schemes for achieving high order accuracy in time. Here we
focus on an implicit multi-stage multi-step method, known in the literature as
Two Implicit Advanced Step-point (TIAS) method, analyzing the performance
of the sixth-order accurate TIAS scheme for long time simulations of sti and
non sti unsteady problems.
The second objective of this work is to demonstrate the applicability and
reliability of optimization algorithms to control spurious numerical oscillations
in simulation of transonic
ows. The proposed optimization strategy relies on
the gradient based optimization approach employing an Automatic Di erentiation (AD) tool for the evaluation of the sensitivities. The optimization
process acts directly on the shock capturing technique, seeking for the optimal
values of the shock capturing parameters.
The performance of the solver is demonstrated by solving several test-cases
of direct relevance in the context of automotive and aerodynamic applications.
The comparison between experimental/analytical and numerical results
allowed the validation and/or revision of physical and numerical models implemented
in the code. Finally, we remark that this work is the starting point of a
larger investigation that aims to deal with ICE
ow conditions that are poorly
predicted by RANS approaches, such as
ow separation and reattachment in
a highly three-dimensional con guration, by using time-accurate integration
of the DG space-discretized ILES and hybrid RANS-LES models.; Università della Calabria 4Soggetto
Macchine a fluido; Fluidodinamica
Relazione
ING/IND-08;