Numerical Airframe Aerodynamic Performance Prediction: An Exergy Point of View
Autor: | Arntz, A., Atinault, O., Destarac, D. |
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Přispěvatelé: | ONERA - The French Aerospace Lab [Meudon], ONERA-Université Paris Saclay (COmUE), Broc, Alain |
Jazyk: | angličtina |
Rok vydání: | 2014 |
Předmět: |
[PHYS.PHYS.PHYS-FLU-DYN]Physics [physics]/Physics [physics]/Fluid Dynamics [physics.flu-dyn]
[PHYS.PHYS.PHYS-FLU-DYN] Physics [physics]/Physics [physics]/Fluid Dynamics [physics.flu-dyn] [PHYS.PHYS.PHYS-SPACE-PH] Physics [physics]/Physics [physics]/Space Physics [physics.space-ph] [PHYS.PHYS.PHYS-SPACE-PH]Physics [physics]/Physics [physics]/Space Physics [physics.space-ph] |
Zdroj: | 49th International Symposium of Applied Aerodynamics 49th International Symposium of Applied Aerodynamics, Mar 2014, LILLE, France |
Popis: | The prediction of the aerodynamic performance of airframe has been historically made via the determination and decomposition of the force opposing the aircraft motion: drag. The paper presents an innovative energy approach which is based on the destruction of exergy by irreversible processes. A required step in the development process is to validate its numerical implementation via various CFD test cases: 2D aerofoil and 3D wing RANS test cases are presented in subsonic and transonic regimes. Mesh convergence studies prove the exergy approach to have a similar accuracy as the traditional near-field drag approach while offering a phenomenological breakdown comparable to a far-field formulation. |
Databáze: | OpenAIRE |
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