Abstract
AbstractThis article presents a methodology whereby adjoint solutions for partitioned multiphysics problems can be computed efficiently, in a way that is completely independent of the underlying physical sub-problems, the associated numerical solution methods, and the number and type of couplings between them. By applying the reverse mode of algorithmic differentiation to each discipline, and by using a specialized recording strategy, diagonal and cross terms can be evaluated individually, thereby allowing different solution methods for the generic coupled problem (for example block-Jacobi or block-Gauss-Seidel). Based on an implementation in the open-source multiphysics simulation and design software SU2, we demonstrate how the same algorithm can be applied for shape sensitivity analysis on a heat exchanger (conjugate heat transfer), a deforming wing (fluid–structure interaction), and a cooled turbine blade where both effects are simultaneously taken into account.
Funder
Bayerische Forschungsstiftung
Technische Universität Kaiserslautern
Publisher
Springer Science and Business Media LLC
Subject
Control and Optimization,Computer Graphics and Computer-Aided Design,Computer Science Applications,Control and Systems Engineering,Software
Reference34 articles.
1. Albring TA, Sagebaum M, Gauger NR (2016) Efficient aerodynamic design using the discrete adjoint method in SU2. In: 17th AIAA/ISSMO multidisciplinary analysis and optimization conference
2. Albring TA, Dick T, Gauger NR (2017) Assessment of the recursive projection method for the stabilization of discrete adjoint solvers. In: 18th AIAA/ISSMO multidisciplinary analysis and optimization conference
3. Biedron RT, Carlson JR, Derlaga JM, Gnoffo PA, Hammond DP, Jones WT, Kleb B, Lee-Rausch EM, Nielsen EJ, Park MA, Rumsey CL, Thomas JL, Thompson KB, Wood WA (2019) Fun3d manual: 13.6. In: NASA TM 2019-220416
4. Burghardt O, Gauger NR, Economon TD (2019) Coupled adjoints for conjugate heat transfer in variable density incompressible flows. In: AIAA Aviation 2019 Forum
5. Campobasso MS, Giles MB (2004) Stabilization of a linear flow solver for turbomachinery aeroelasticity using recursive projection method. AIAA J 42(9):1765–1774
Cited by
5 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献