2023
DOI: 10.1093/jcde/qwac140
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Separable shape tensors for aerodynamic design

Abstract: Airfoil shape design is a classical problem in engineering and manufacturing. In this work, we combine principled physics-based considerations for the shape design problem with modern computational techniques using a data-driven approach. Modern and traditional analyses of 2D and 3D aerodynamic shapes reveal a flow-based sensitivity to specific deformations that can be represented generally by affine transformations (rotation, scaling, shearing, translation). We present a novel representation of shapes that de… Show more

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Cited by 5 publications
(2 citation statements)
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“…G2Aero implements the novel separable tensor framework outlined in detail in Grey et al (2023). It is designed to learn matrix-submanifolds, generate novel shapes localized to data, control shape undulations by truncating an ordered basis of deforming modes, and enable a novel notion of "consistent deformations" as an approach to regularized surface design.…”
Section: Methodsmentioning
confidence: 99%
“…G2Aero implements the novel separable tensor framework outlined in detail in Grey et al (2023). It is designed to learn matrix-submanifolds, generate novel shapes localized to data, control shape undulations by truncating an ordered basis of deforming modes, and enable a novel notion of "consistent deformations" as an approach to regularized surface design.…”
Section: Methodsmentioning
confidence: 99%
“…The left side of Figure 1 showed that a six-rotor drone and air flows are augmented in an office room shown by an MR device, and the right side demonstrates that an extracted wing section called airfoil which is very critical in the wing performance produces aerodynamic lifting and drag forces. Although airfoil shape design is a classical subject in engineering and manufacturing, it is still being studied by many researchers such as Grey et al [20] and Wang et al [21]. Wing design analysis is generally accompanied by CFD simulation around the airfoils belonging to the given wing.…”
Section: Introductionmentioning
confidence: 99%