• Login
    View Item 
    •   DSpace Home
    • ASME
    • Journal of Turbomachinery
    • View Item
    •   DSpace Home
    • ASME
    • Journal of Turbomachinery
    • View Item
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Data Assimilation of Transitional and Separated Turbomachinery Flows With Physics-Informed Neural Networks

    Thumbnail
    View/Open
    turbo-24-1059.pdf (8.315Mb)
    Date
    2025
    Author
    Hanrahan, Sean K.
    Kozul, Melissa
    Sandberg, Richard D.
    Metadata
    Show full item record
    Abstract
    Despite the demonstrated utility of Reynolds-averaged Navier–Stokes (RANS) calculations for many industrially relevant problems, the method yields unsatisfactory representations of many flows of engineering interest, such as nonequilibrium turbulence, massive flow separation, coherent unsteadiness, and secondary flow features. Due to the Reynolds-averaging process, a turbulence model is required to close the RANS equations, and the simple physical arguments and approximations used in many turbulence models can cause erroneous results when applied to the flows that feature strong pressure gradients, sudden changes in mean-strain-rate, surface curvature, and turbulence anisotropy. Physics-informed neural networks (PINNs) offer a way to model aerodynamic problems without explicitly requiring turbulence closure. The network can use sparse training data and unclosed RANS equations to reconstruct the flow without a turbulence model. In this work, PINNs are applied to two problems of relevance in the turbomachinery community. First, we consider a variable area channel known as the periodic hills, which features a shear layer, a separation bubble, as well as favorable and adverse pressure gradients. Second, a PINN is applied to the T106C low-pressure turbine blade with two different levels of inlet turbulence intensity, featuring the additional challenges of transition and laminar separation. We demonstrate that PINNs are capable of modeling wall-bounded quantities such as Cf and Cp in such complex flows, capturing sensitive features such as the change in separation length when the turbulent inlet conditions are altered. This article undertakes a considered and pragmatic assessment of the state of PINNs when applied to complex high Reynolds number flows, highlighting where the method is comparable to the quality of high-fidelity simulations, and conversely where the method degrades with a lack of training data around regions of interest.
    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4310123
    Collections
    • Journal of Turbomachinery

    DSpace software copyright © 2002-2015  DuraSpace
    Contact Us | Send Feedback
    Theme by 
    @mire NV
     

     

    Browse

    All of DSpaceCommunities & CollectionsBy Issue DateAuthorsTitlesSubjectsThis CollectionBy Issue DateAuthorsTitlesSubjects

    My Account

    LoginRegister

    Statistics

    View Usage Statistics

    DSpace software copyright © 2002-2015  DuraSpace
    Contact Us | Send Feedback
    Theme by 
    @mire NV