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Model Order Reduction using POD

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AEROSPACE COMPUTATIONAL DESIGN LABORATORY. Model Order Reduction using POD ... Through the use of model order reduction, lower order models can be generated ... – PowerPoint PPT presentation

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Title: Model Order Reduction using POD


1
Model Order Reduction using POD
  • Student Researcher Tony Lau
  • Advisor Karen Willcox
  • Motivation
  • It is difficult to resolve the mean flow
    characteristics and capture the inherent
    unsteadiness of an aerodynamic flow.
  • Project Goals
  • Through the use of model order reduction, lower
    order models can be generated that require less
    computational power yet retain the high level of
    fidelity of a full order solver.
  • Proper Orthogonal Decomposition (POD) is the
    technique used to create the reduced order models.

2
Model Order Reduction using POD
  • Solutions generated from flow simulations may
    contain an extensive number of states.
  • Flow simulations are performed using NASAs
    FUN2D, a fully unstructured Navier-Stokes solver
  • Solution states ( ) may number on
    the order of 106 for a solution as shown here.
  • Large and complex simulationsare very
    computationally costly
  • Analyzing variations in the flow, such as
    changing initial conditions, each require a
    completely new simulation

3
Model Order Reduction using POD
  • Application of Model Order Reduction
  • Snapshots of the flow are taken from the full
    order solver.
  • These snapshots are solutions of the
    computational model at different instances in
    time.
  • Proper Orthogonal Decomposition
  • The proper orthogonal decomposition determines
    an optimal set of basis vectors that minimize
    the error between the exact and projected data.
  • Reduction achieved may be ofseveral orders of
    magnitude
  • This reduced model may be used for further
    studies, but at a lower computational cost.
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