On the characteristic structure of the adjoint Euler equations and the analytic adjoint solution of supersonic inviscid flows
arXiv:2503.13007 · doi:10.3390/aerospace12060494
Abstract
The characteristic structure of the two-dimensional adjoint Euler equations is examined. The behavior is similar to that of the original Euler equations, but with the information travelling in the opposite direction. The compatibility conditions obeyed by the adjoint variables along characteristic lines are derived. It is also shown that adjoint variables can have discontinuities across characteristics and the corresponding jump conditions are obtained. It is shown how this information can be used to obtain exact predictions for the adjoint variables, particularly for supersonic flows. The approach is illustrated by the analysis of supersonic flow past a double wedge airfoil, for which an analytic adjoint solution is obtained in the near-wall region. The solution is zero downstream of the airfoil and piecewise constant around it except across the expansion fan, where the adjoint variables change smoothly while remaining constant along each Mach wave within the fan.
arXiv comment28 pages, revised, post-refereeing version to be published in Aerospace
References in corpus (6)
- Continuous Adjoint Complement to the Blasius Equation
- Entropy and Adjoint Methods
- Exact inviscid drag adjoint solution for subcritical flows
- Analytic adjoint solution for incompressible potential flows
- Shock equations and jump conditions for the 2D Adjoint Euler equations
- Explaining the Lack of Mesh Convergence of Inviscid Adjoint Solutions Near Solid Walls for Subcritical Flows