TL;DR
This paper investigates dimension reduction techniques for turbomachinery CFD simulations, demonstrating that subspaces are consistent across blades and proposing a polynomial variable projection method for efficient identification of these subspaces, aiding design comparison.
Contribution
It introduces a novel polynomial variable projection approach for dimension reduction in turbomachinery simulations, improving efficiency over existing statistical methods.
Findings
Subspaces are largely independent of Mach and Reynolds numbers across blades.
Polynomial variable projection accurately identifies dimension reducing subspaces.
Designs with balanced performance can be visually selected using these subspaces.
Abstract
Motivated by the idea of turbomachinery active subspace performance maps, this paper studies dimension reduction in turbomachinery 3D CFD simulations. First, we show that these subspaces exist across different blades---under the same parametrization---largely independent of their Mach number or Reynolds number. This is demonstrated via a numerical study on three different blades. Then, in an attempt to reduce the computational cost of identifying a suitable dimension reducing subspace, we examine statistical sufficient dimension reduction methods, including sliced inverse regression, sliced average variance estimation, principal Hessian directions and contour regression. Unsatisfied by these results, we evaluate a new idea based on polynomial variable projection---a non-linear least squares problem. Our results using polynomial variable projection clearly demonstrate that one can…
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