Add to ORKGThis paper describes the derivation and implementation of the discrete adjoint equations based on frequency domain methods (linear harmonics and harmonic balance) within a turbomachinery CFD code. Applications to model problems are presented which demonstrate the potential of the method for multidisciplinary turbomachinery problems, e.g. aeroelastics or aeroacoustics
This paper summarizes work done within the framework of an adjoint multidisciplinary optimization fo...
Shape optimization in unsteady flow problems enables the consideration of dynamic effects on design....
The present paper investigates a time-domain harmonic balance method as an alternative to classical ...
This paper describes the derivation and implementation of the discrete adjoint equations based on f...
This paper describes the development and initial application of an adjoint harmonic balance solver. ...
This contribution describes the development of a discrete adjoint solver for the harmonic balance me...
The analysis of aeroelastic properties is an important aspect in the design of turbomachinery compon...
This paper presents an overview of the steady and harmonic adjoint methods for turbomachinery design...
This paper presents an adjoint analysis for three-dimensional unsteady. viscous flows aimed at the c...
An overview is presented of the steady and harmonic adjoint methods for turbomachinery design using ...
In recent years, there has been rapid progress in aerodynamic optimization methods which use adjoint...
This paper demonstrates how the worksum output produced by the linear harmonic ow analysis can be ob...
The possibility of taking into account unsteady flow effects if performing turbomachinery shape opti...
This paper discusses the use of both steady and unsteady discrete adjoint methods for the design of ...
Turbomachinery blades characterized by highly-loaded, slender profiles and operating under unsteady ...
This paper summarizes work done within the framework of an adjoint multidisciplinary optimization fo...
Shape optimization in unsteady flow problems enables the consideration of dynamic effects on design....
The present paper investigates a time-domain harmonic balance method as an alternative to classical ...
This paper describes the derivation and implementation of the discrete adjoint equations based on f...
This paper describes the development and initial application of an adjoint harmonic balance solver. ...
This contribution describes the development of a discrete adjoint solver for the harmonic balance me...
The analysis of aeroelastic properties is an important aspect in the design of turbomachinery compon...
This paper presents an overview of the steady and harmonic adjoint methods for turbomachinery design...
This paper presents an adjoint analysis for three-dimensional unsteady. viscous flows aimed at the c...
An overview is presented of the steady and harmonic adjoint methods for turbomachinery design using ...
In recent years, there has been rapid progress in aerodynamic optimization methods which use adjoint...
This paper demonstrates how the worksum output produced by the linear harmonic ow analysis can be ob...
The possibility of taking into account unsteady flow effects if performing turbomachinery shape opti...
This paper discusses the use of both steady and unsteady discrete adjoint methods for the design of ...
Turbomachinery blades characterized by highly-loaded, slender profiles and operating under unsteady ...
This paper summarizes work done within the framework of an adjoint multidisciplinary optimization fo...
Shape optimization in unsteady flow problems enables the consideration of dynamic effects on design....
The present paper investigates a time-domain harmonic balance method as an alternative to classical ...