Aerospace Validation Case

ARA M100 Wingbody

Envenio routinely runs cases to validate the performance and accuracy of its engineering models and equations. One of our engineers ran a CFD simulation using our EXN/AERO solver using 4 CPUs and 3 GPUs. The ARA M100 wing body geometry is based on a scale wind tunnel model and is referenced by NASA as a validation case for CFD codes with compressible / transonic flow capability. The configuration of the model is similar to what is seen in civil and military transport aviation and features a finite wing, a realistic wing root and a fuselage

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