| Popis: |
The aerodynamic analysis by the exergy method is a powerful approach which allows establishing the theoretical limits of the aerodynamic performance of a given body, based on an aero-thermodynamic approach. The most used formulation is the Arntz’s method [1], which is well suited for the analysis of CFD data. This formulation was widely applied and validated for plenty of test cases but all of them were high-aspect ratio configurations. Then, the objective of this work is to study a test case with low aspect ratio: a delta wing with 74° of sweep angle, which is characterized by extreme flow features like strong vortices. It was found that the exergy formulation behaves well even under such challenging conditions. However, the related extreme flowfield allows identifying some hard points like the wake-reduced exergy analysis of the vortex breakdown, the impact of the solver setting on the final assessment, the viscous anergy generation, among other topics. |
