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Descripción
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| Optimal aerodynamic shape design aims to find the minimum of a functional that de- scribes an aerodynamic characteristic, by controlling the PDE modelling the dynamics of the flow that surrounds an aircraft, by using surface deformation techniques. As a solution to the enormous computational resources required for classical shape optimization of func- tionals of aerodynamic interest, probably the best strategy is to apply methods inspired in control theory. One of the key ingredients relies on the usage of the adjoint methodology in order to simplify the computation of gradients. In this paper we will restrict our attention to optimal shape design in two dimensional systems governed by the steady Euler equations for flows whose steady-state solutions present discontinuities in the flow variables (an isolated shock wave) | |
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Internacional
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Si |
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JCR del ISI
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Si |
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Título de la revista
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AIAA JOURNAL |
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ISSN
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0001-1452 |
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Factor de impacto JCR
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1,025 |
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Información de impacto
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Volumen
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47 |
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DOI
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Número de revista
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3 |
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Desde la página
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552 |
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Hasta la página
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562 |
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Mes
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MARZO |
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Ranking
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