rijke stands for Rijke tube and tswc stands for turbulent swirl combustor. mesh_*.xml contains the mesh in xml format. p_dir_*.xml and p_adj_*.xml contain the direct and adjoint fields in xml format. omega_*.txt contains the eigenvalue. my_dict_*.pickle contains the control points and the shape derivatives as byte streams. The dataset also contains the pvd (ParaView Data) files for the amplitude and phase of the direct and adjoint fields
This paper addresses the aeroacoustic shape optimization of a 3D aero-engine intake by means of grad...
An adjoint system of the Euler equations of gas dynamics is derived in order to solve aerodynamic sh...
Lean combustion technologies in gas turbines reduce the generation of NOx but increase the susceptib...
Abstract Thermoacoustic instabilities, which arise due to the interaction between fla...
This paper proposes a method for shape optimization in aero-acoustics and applies it to a Helmholtz ...
International audienceHadamard's method of shape differentiation is applied to topology optimization...
International audienceThe simulation process of CFD is usually starting from a CAD model. Due to the...
We propose a method that allows the computation of the continuous adjoint network system based on th...
An adjoint-based shape optimization approach for supersonic turbine cascades is proposed for applic...
Industrial design developments are more and more assisted by computer optimization algorithms to spe...
The aim of this paper is to present the adjoint equations for shape optimization derived from steady...
We construct a low-order thermoacoustic network model that contains the most influential physical me...
Aerodynamic shape optimisation with gradient-based methods is rapidly gaining popularity in the aero...
Gas turbines and rocket engines sometimes suffer from violent oscillations caused by feedback betwee...
In gas turbines, thermoacoustic oscillations grow if moments of high fluctuating heat release rate c...
This paper addresses the aeroacoustic shape optimization of a 3D aero-engine intake by means of grad...
An adjoint system of the Euler equations of gas dynamics is derived in order to solve aerodynamic sh...
Lean combustion technologies in gas turbines reduce the generation of NOx but increase the susceptib...
Abstract Thermoacoustic instabilities, which arise due to the interaction between fla...
This paper proposes a method for shape optimization in aero-acoustics and applies it to a Helmholtz ...
International audienceHadamard's method of shape differentiation is applied to topology optimization...
International audienceThe simulation process of CFD is usually starting from a CAD model. Due to the...
We propose a method that allows the computation of the continuous adjoint network system based on th...
An adjoint-based shape optimization approach for supersonic turbine cascades is proposed for applic...
Industrial design developments are more and more assisted by computer optimization algorithms to spe...
The aim of this paper is to present the adjoint equations for shape optimization derived from steady...
We construct a low-order thermoacoustic network model that contains the most influential physical me...
Aerodynamic shape optimisation with gradient-based methods is rapidly gaining popularity in the aero...
Gas turbines and rocket engines sometimes suffer from violent oscillations caused by feedback betwee...
In gas turbines, thermoacoustic oscillations grow if moments of high fluctuating heat release rate c...
This paper addresses the aeroacoustic shape optimization of a 3D aero-engine intake by means of grad...
An adjoint system of the Euler equations of gas dynamics is derived in order to solve aerodynamic sh...
Lean combustion technologies in gas turbines reduce the generation of NOx but increase the susceptib...