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Hauptverfasser: Zhang, Yanbing, Yuan, Ruifeng, Wu, Lei
Format: Preprint
Veröffentlicht: 2025
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Online-Zugang:https://arxiv.org/abs/2511.18433
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author Zhang, Yanbing
Yuan, Ruifeng
Wu, Lei
author_facet Zhang, Yanbing
Yuan, Ruifeng
Wu, Lei
contents Adjoint based shape optimization is a powerful technique in fluid-dynamics optimization, capable of identifying an optimal shape within only dozens of design iterations. However, when extended to rarefied gas flows, the computational cost becomes enormous because both the six dimensional primal and adjoint Boltzmann equations must be solved for each candidate shape. Building on the general synthetic iterative scheme (GSIS) for solving the primal Boltzmann model equation, this paper presents a fast converging and asymptotic preserving method for solving the adjoint kinetic equation. The GSIS accelerates the convergence of the adjoint kinetic equation by incorporating solutions of macroscopic synthetic equations, whose constitutive relations include the Newtonian stress law along with higher order terms capturing rarefaction effects. As a result, the method achieves asymptotic preservation (allowing the use of large spatial cell sizes in the continuum limit) while maintaining accuracy in highly rarefied regimes. Numerical tests demonstrate exceptional performance on drag minimization problems for 3D bodies, achieving drag reductions of 34.5% in the transition regime and 61.1% in the slip-flow regime within roughly ten optimization iterations. For each candidate shape, converged solutions of the primal and adjoint Boltzmann equation are obtained with only a few dozen updates of the velocity distribution function, dramatically reducing computational cost compared with conventional methods.
format Preprint
id arxiv_https___arxiv_org_abs_2511_18433
institution arXiv
publishDate 2025
record_format arxiv
spellingShingle A fast-converging and asymptotic-preserving method for adjoint shape optimization of rarefied gas flows
Zhang, Yanbing
Yuan, Ruifeng
Wu, Lei
Computational Physics
Adjoint based shape optimization is a powerful technique in fluid-dynamics optimization, capable of identifying an optimal shape within only dozens of design iterations. However, when extended to rarefied gas flows, the computational cost becomes enormous because both the six dimensional primal and adjoint Boltzmann equations must be solved for each candidate shape. Building on the general synthetic iterative scheme (GSIS) for solving the primal Boltzmann model equation, this paper presents a fast converging and asymptotic preserving method for solving the adjoint kinetic equation. The GSIS accelerates the convergence of the adjoint kinetic equation by incorporating solutions of macroscopic synthetic equations, whose constitutive relations include the Newtonian stress law along with higher order terms capturing rarefaction effects. As a result, the method achieves asymptotic preservation (allowing the use of large spatial cell sizes in the continuum limit) while maintaining accuracy in highly rarefied regimes. Numerical tests demonstrate exceptional performance on drag minimization problems for 3D bodies, achieving drag reductions of 34.5% in the transition regime and 61.1% in the slip-flow regime within roughly ten optimization iterations. For each candidate shape, converged solutions of the primal and adjoint Boltzmann equation are obtained with only a few dozen updates of the velocity distribution function, dramatically reducing computational cost compared with conventional methods.
title A fast-converging and asymptotic-preserving method for adjoint shape optimization of rarefied gas flows
topic Computational Physics
url https://arxiv.org/abs/2511.18433