Adjoint and Direct Characteristic Equations for Two-Dimensional Compressible Euler Flows

Author:

Ancourt Kevin1,Peter Jacques1ORCID,Atinault Olivier2

Affiliation:

1. Département Aérodynamique, Aéroélasticité et Acoustique (DAAA), ONERA, Université Paris Saclay, 29 Avenue de la Division Leclerc, Châtillon, 92322 Paris, France

2. Département Aérodynamique, Aéroélasticité et Acoustique (DAAA), ONERA, Université Paris Saclay, 8 Rue des Vertugadins, 92190 Meudon, France

Abstract

The method of characteristics is a classical method for gaining understanding in the solution of a partial differential equation. It has recently been applied to the adjoint equations of the 2D steady-state Euler equations and the first goal of this paper is to present a linear algebra analysis that greatly simplifies the discussion of the number of independent characteristic equations satisfied along a family of characteristic curves. This method may be applied for both the direct and the adjoint problem. Our second goal is to directly derive in conservative variables the characteristic equations of 2D compressible inviscid flows. Finally, the theoretical results are assessed for a nozzle flow with a classical scheme and its dual consistent discrete adjoint.

Funder

European Union’s Horizon 2020 research and innovation program

SONICE project

French Directorate General for Civil Aviation

Publisher

MDPI AG

Subject

Aerospace Engineering

Reference45 articles.

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2. Shapiro, A. (1954). The Dynamics and Thermodynamics of Compressible Fluid Flow, The Ronald Press Company.

3. Bonnet, A., and Luneau, J. (1989). Aérodynamique. Théories de la Dynamique des Fluides, Cepadues.

4. Délery, J. (2008). Traité D’aérodynamique Compressible, Collection Mécanique des Fluides, Lavoisier—Hermés, Science.

5. Aerodynamic design via control theory;Jameson;J. Sci. Comput.,1988

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