Aerospace

Validation: ARA-M100 Version 1.0 Applications Transonic Aerodynamics External Aircraft Component Design Models active in this Validation Case Compressible flow Energy models Ideal gases Mixed Precision Objective To profile the accuracy and performance of Envenio’s EXN/AERO manycore CFD solver on a challenging transonic aerospace test case. We undertook this demonstration to show that DES and LES are…

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Applications Transonic Aerodynamics External Aircraft Component Design Models active in this Validation Case Compressible flow Energy models Ideal gases Double Precision Objective To profile the accuracy and performance of Envenio’s EXN/AERO manycore CFD solver on a challenging transonic aerospace test case. Reference Case Description – ARA-M100 Wingbody The ARA M100 wing body geometry is based…

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Applications Supersonic Aerodynamics Transonic Aerodynamics External Aircraft Component Design Models active in this Validation Case Compressible flow Energy models Ideal gases Double Precision Objective To understand the accuracy of Envenio’s EXN/AERO manycore CFD solver in the context of an aerospace wing study. Reference Case Description – ONERA Wing The ONERA M6 wing geometry is based…

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