Adjoint based methods have become the focus of research in CFD optimization pertaining to their low computational cost compared to other traditional methods. In principle, adjoints are computed via two methods: Continuous and Discrete. In the continuous method, adjoints are computed by deriving the adjoint equations of corresponding state variables and boundary conditions and then are solved using similar schemes as that of the primal. The discrete approach using Algorithmic Differentiation (AD) [9] is implemented either by source transformation or by an operator overloading tool. For an object-oriented code in C++ like OpenFOAM [10], the use of an operator overloading tool becomes imperative. Discrete adjoints based on operator overloading...
Aerodynamic sensitivity analysis codes are developed via the hand-differentiation using a direct dif...
This paper presents an implementation of discrete adjoint solver using an automatic differentiation ...
A discrete adjoint method is developed and demonstrated for aerodynamic design optimization on unstr...
Sensitivity analysis with the aim of design optimization is a growing area of interest in Computatio...
<p>Sensitivity analysis with the aim of design optimization is a growing area of interest in Computa...
AbstractWe present a discrete adjoint version of the open-source fluid-dynamics package OpenFOAM obt...
Aim: Solution of the incompressible Navier-Stokes equations •Problem: No inherent coupling for the c...
<p>Adjoint based calculation of sensitivities pertaining to a Computational Fluid Dynamics (CFD) Sol...
Methods and computing hardware advances have enabled accurate predictions of complex compressible tu...
The complete discrete adjoint equations for an unstructured finite volume compressible Navier-Stokes...
Shape optimization of modern three-dimensional hypersonic inlets requires many geometric design para...
<p>Adjoint methods allow to compute the gradient of a cost function at an expense that is independen...
PhD, 156ppThis thesis investigates stabilisation of the SIMPLE-family discretisations for incompress...
This study seeks to reduce the degree of uncertainty that often arises in computational fluid dynami...
We propose a method for selectively applying automatic differentiation (AD) by operator overloading ...
Aerodynamic sensitivity analysis codes are developed via the hand-differentiation using a direct dif...
This paper presents an implementation of discrete adjoint solver using an automatic differentiation ...
A discrete adjoint method is developed and demonstrated for aerodynamic design optimization on unstr...
Sensitivity analysis with the aim of design optimization is a growing area of interest in Computatio...
<p>Sensitivity analysis with the aim of design optimization is a growing area of interest in Computa...
AbstractWe present a discrete adjoint version of the open-source fluid-dynamics package OpenFOAM obt...
Aim: Solution of the incompressible Navier-Stokes equations •Problem: No inherent coupling for the c...
<p>Adjoint based calculation of sensitivities pertaining to a Computational Fluid Dynamics (CFD) Sol...
Methods and computing hardware advances have enabled accurate predictions of complex compressible tu...
The complete discrete adjoint equations for an unstructured finite volume compressible Navier-Stokes...
Shape optimization of modern three-dimensional hypersonic inlets requires many geometric design para...
<p>Adjoint methods allow to compute the gradient of a cost function at an expense that is independen...
PhD, 156ppThis thesis investigates stabilisation of the SIMPLE-family discretisations for incompress...
This study seeks to reduce the degree of uncertainty that often arises in computational fluid dynami...
We propose a method for selectively applying automatic differentiation (AD) by operator overloading ...
Aerodynamic sensitivity analysis codes are developed via the hand-differentiation using a direct dif...
This paper presents an implementation of discrete adjoint solver using an automatic differentiation ...
A discrete adjoint method is developed and demonstrated for aerodynamic design optimization on unstr...