Efficient sequential reliability-based design optimization with adaptive kriging inverse reliability analysis

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Abstract/Contents

Abstract
In this thesis, new methods for reliability-based design optimization (RBDO) are presented. The Adaptive Kriging Inverse Reliability Analysis (AKIRA) algorithm and a multifidelity sequential RBDO algorithm are introduced and demonstrated on a complex multidisciplinary supersonic nozzle design problem. AKIRA demonstrates competitive performance with other reliability analysis algorithms while also benefiting from the solution of the inverse reliability analysis problem during RBDO. The proposed sequential RBDO algorithm mitigates the cost of solving the RBDO problem by decoupling the optimization and reliability analyses, thereby reducing its solution to a series of deterministic optimizations. The method is motivated by anchored decomposition, has guaranteed convergence inherited from trust region methods, and is shown in certain cases to be a generalization of existing sequential RBDO methods. It also derives enhanced efficiency by incorporating lower-fidelity models when available. The final demonstration of the proposed algorithms on an industrial-type problem, the supersonic nozzle, shows that the solution of RBDO problems for complex realistic engineering applications is well within reach.

Description

Type of resource text
Form electronic resource; remote; computer; online resource
Extent 1 online resource.
Place California
Place [Stanford, California]
Publisher [Stanford University]
Copyright date 2018; ©2018
Publication date 2018; 2018
Issuance monographic
Language English

Creators/Contributors

Author Fenrich, Richard Walter
Degree supervisor Alonso, Juan José, 1968-
Thesis advisor Alonso, Juan José, 1968-
Thesis advisor Iaccarino, Gianluca
Thesis advisor Kochenderfer, Mykel J, 1980-
Degree committee member Iaccarino, Gianluca
Degree committee member Kochenderfer, Mykel J, 1980-
Associated with Stanford University, Department of Aeronautics and Astronautics.

Subjects

Genre Theses
Genre Text

Bibliographic information

Statement of responsibility Richard Walter Fenrich.
Note Submitted to the Department of Aeronautics and Astronautics.
Thesis Thesis Ph.D. Stanford University 2018.
Location electronic resource

Access conditions

Copyright
© 2018 by Richard Walter Fenrich
License
This work is licensed under a Creative Commons Attribution 3.0 Unported license (CC BY).

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