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Fluid mechanics / Shape optimization / Computational fluid dynamics / Mathematical analysis / Fluid dynamics / Aerodynamics / Navier–Stokes equations / Dynamics


  http://su2.stanford.edu Inviscid & RANS sensitivity computation, and optimal aerodynamic shape design
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Document Date: 2014-06-17 15:53:41

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File Size: 2,91 MB

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Adjoint / /

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S3 Swiss Space Systems / Aerospace Design Laboratory / /

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Aerospace Design Laboratory / Stanford University / /

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opensource tool / open-source software suite / online forum / /

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Microsoft Windows / GNU / Mac OS X / Linux / /

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National Aeronautics and Space Administration / Stanford University / /

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Python / C++ / /

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Stanford University / /

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simulation / Linux / /

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http /

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