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作者机构:Stanford Univ Dept Aeronaut & Astronaut Stanford CA 94305 USA Stanford Univ Dept Mech Engn Stanford CA 94305 USA Stanford Univ Inst Computat & Math Engn Stanford CA 94305 USA
出 版 物:《SIAM JOURNAL ON SCIENTIFIC COMPUTING》 (工业与应用数学会科学计算杂志)
年 卷 期:2022年第44卷第4期
页 面:A2176-A2203页
核心收录:
学科分类:07[理学] 070104[理学-应用数学] 0701[理学-数学]
基 金:Boeing Company Office of Naval Research [N00014-17-1-2749] Air Force Office of Scientific Research [FA9550-20-1-0358]
主 题:active subspace gradient-based optimization hyperreduction nonlinear model reduction parameter sampling PDE-constrained optimization
摘 要:This paper introduces the concept of a database of piecewise-global, nonlinear, projection-based reduced-order models and intertwines it with that of an active subspace. The result is a computational framework for accelerating the solution of optimization problems in a design parameter space of a relatively large dimension. On the algorithmic side, the scope of this framework includes multistart, gradient-based optimization methods and hyperreduced nonlinear models. On the application side, it includes multi-objective and global optimization problems, as well as nonlinear, PDE-based constraints. The potential of the proposed computational framework for optimization is demonstrated using aerodynamic shape optimization problems associated with two different flight systems: the flying wing aircraft mAEWing2, and the NASA Common Research Model (CRM) for transport aircraft.