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Mesh generation / Aerodynamics / Aerospace engineering / Fluid dynamics / Physics / Spatial twist continuum / Computational fluid dynamics / Computational science / Science


Department of Aeronautics Imperial College London PhD Studentship The Impact of Boundary Representation and Mesh Quality on the Performance of High-Order Accurate Flow Solvers for Complex Aerodynamic Flows Tax-free stip
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Document Date: 2014-10-15 04:31:27

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File Size: 59,85 KB

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Aeronautics Imperial College / Imperial College / Stanford University / /

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aerodynamic flow solutions / /

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Imperial College / National Aeronautics and Space Administration / Stanford University / /

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Peter Vincent / /

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Python / C++ / /

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Stanford University / /

Technology

CFD algorithms / simulation / /

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