Aerodynamic Shape Optimization Starting From Random Initial Geometry

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Reference Important Context

Video showing computational grids used while optimising axisymmetric nose cones in hypersonic flow. This is a demonstration of our mesh deformation algorithm, which was developed for

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Quick reference points

• Video showing computational grids used while optimising axisymmetric nose cones in hypersonic flow.
• This is a demonstration of our mesh deformation algorithm, which was developed for

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