This paper shows the application of the aerodynamics exergy analysis preliminary formulation developed for unsteady flows for adiabatic and fixed bodies under low subsonic flow conditions (no shock-waves). The numerical implementation for URANS CFD cases of the presented formulation is explained. The test case is a circular cylinder in vortex shedding regime at Reynolds number 140, at low subsonic flow, with no movement with respect to the reference frame. The validation of the developed formulation is done by comparing the drag coefficient computed by the presented unsteady exergy formulation versus the near field drag coefficient taken as reference
The interaction between the wake of a rotor blade and a downstream cylinder holds the key to the und...
Unsteady flows are very common in nature. Birds, insects, fish and other animals predominantly rely...
The paper addresses the applicability of unsteady Reynolds-Averaged Navier-Stokes CFD methods for th...
This paper shows the application of the aerodynamics exergy analysis preliminary formulation develo...
This paper aims to provide a prediction method for the transverse exergy of the wing’s trailing vort...
The aerodynamic analysis by the exergy method is reviewed. The existing formulations are analyzed fo...
The aerodynamic analysis by the exergy method is a powerful approach which allows establishing the t...
International audienceAircraft have evolved into extremely complex systems that require adapted meth...
The application of exergy analysis to aerospace systems requires proper analysis of the entropy gene...
More and more often computer simulations of airflow are used as a tool in aircraft design. In this r...
The paper considers the results of analyzing the aerodynamics and heat exchange of a fixed cylinder ...
Unsteady Reynolds-averaged Navier-Stokes (URANS) simulations and detached-eddy simulations (DES) wer...
International audienceThis paper aims to perform an analysis of the flow field around an airfoil by ...
A new exergy-based formulation is derived for the assessment of the aerothermopropulsive performance...
Incompressible, viscous, two-dimensional unsteady flows over bluff bodies are simulated via the use ...
The interaction between the wake of a rotor blade and a downstream cylinder holds the key to the und...
Unsteady flows are very common in nature. Birds, insects, fish and other animals predominantly rely...
The paper addresses the applicability of unsteady Reynolds-Averaged Navier-Stokes CFD methods for th...
This paper shows the application of the aerodynamics exergy analysis preliminary formulation develo...
This paper aims to provide a prediction method for the transverse exergy of the wing’s trailing vort...
The aerodynamic analysis by the exergy method is reviewed. The existing formulations are analyzed fo...
The aerodynamic analysis by the exergy method is a powerful approach which allows establishing the t...
International audienceAircraft have evolved into extremely complex systems that require adapted meth...
The application of exergy analysis to aerospace systems requires proper analysis of the entropy gene...
More and more often computer simulations of airflow are used as a tool in aircraft design. In this r...
The paper considers the results of analyzing the aerodynamics and heat exchange of a fixed cylinder ...
Unsteady Reynolds-averaged Navier-Stokes (URANS) simulations and detached-eddy simulations (DES) wer...
International audienceThis paper aims to perform an analysis of the flow field around an airfoil by ...
A new exergy-based formulation is derived for the assessment of the aerothermopropulsive performance...
Incompressible, viscous, two-dimensional unsteady flows over bluff bodies are simulated via the use ...
The interaction between the wake of a rotor blade and a downstream cylinder holds the key to the und...
Unsteady flows are very common in nature. Birds, insects, fish and other animals predominantly rely...
The paper addresses the applicability of unsteady Reynolds-Averaged Navier-Stokes CFD methods for th...
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