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    A modular matrix-free approach to multidisciplinary design optimization

    Author
    Dener, Alp
    View/Open
    178844_Dener_rpi_0185E_11175.pdf (4.335Mb)
    Other Contributors
    Hicken, Jason; Oberai, Assad; Sahni, Onkar; Mitchell, John E.;
    Date Issued
    2017-12
    Subject
    Aeronautical engineering
    Degree
    PhD;
    Terms of Use
    This electronic version is a licensed copy owned by Rensselaer Polytechnic Institute, Troy, NY. Copyright of original work retained by author.;
    Metadata
    Show full item record
    URI
    https://hdl.handle.net/20.500.13015/2143
    Abstract
    In this thesis, we propose a reduced-space inexact-Newton-Krylov (RSNK) algorithm that can address the challenges posed by the IDF formulation. RSNK achieves this with three key components: a matrix-free formulation that avoids explicit Jacobians and Hessians, a new Krylov solver tailored for nonconvex saddle-point problems, and a novel matrix-free preconditioner for the IDF architecture. We implement RSNK in a parallel-agnostic optimization library, and verify its efficacy on a range of low- and high-fidelity test problems drawn from aerospace applications. Our findings demonstrate that RSNK scales favorably with the size of the design space, exhibits superlinear asymptotic convergence, and can efficiently solve large-scale PDE-governed MDO problems.; Despite its advantages in modularity, the IDF architecture has remained largely unused by researchers and practitioners alike since its introduction in the early 1990s. The addition of large numbers of variables and constraints into the optimization problem proved to be challenging for conventional gradient-based optimization approaches. In particular, the explicit constraint Jacobian required by these algorithms is prohibitively expensive to compute for IDF problems.; The individual discipline feasible (IDF) formulation is a multidisciplinary design optimization (MDO) architecture that provides modularity for the underlying discipline solvers. Similar to reduced-space methods, the IDF formulation does not require the optimization algorithm to converge the state variables for each discipline in addition to the optimization variables; the state equations are still solved fully at each optimization iteration. However, IDF decouples the discipline equations from each other through the introduction of coupling variables and constraints to the optimization problem. Consequently, the discipline solutions at each optimization iteration can be performed independently and in parallel. This promotes the use of existing discipline-specific PDE solvers, and lowers the software development challenge of creating efficient coupled discipline analyses.;
    Description
    December 2017; School of Engineering
    Department
    Dept. of Mechanical, Aerospace, and Nuclear Engineering;
    Publisher
    Rensselaer Polytechnic Institute, Troy, NY
    Relationships
    Rensselaer Theses and Dissertations Online Collection;
    Access
    Restricted to current Rensselaer faculty, staff and students. Access inquiries may be directed to the Rensselaer Libraries.;
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