Verification And Validation Of Cfd Software By Onera, Dlr, Airbus For Helicopter Fuselages

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dc.contributor.authorRottmann, L.
dc.date.accessioned2026-08-13T14:17:22Z
dc.date.issued2024
dc.description.abstractAn extended stencil in Green-Gauss reconstruction and the matrix-free GMRES block Jacobi method are recent advances in CFD, which have been implemented into the new CFD software by ONERA, DLR and Airbus (CODA). The GOAHEAD helicopter fuselage configuration, which was measured in the wind tunnel, is computed with CODA and compared against results generated with DLR's legacy flow solvers FLOWer and TAU.
dc.identifier.citationPresented at 50th European Rotorcraft Forum (ERF 2024), September 10-12, 2024, Marseille, France.
dc.identifier.urihttps://hdl.handle.net/20.500.11881/4579
dc.language.isoen
dc.titleVerification And Validation Of Cfd Software By Onera, Dlr, Airbus For Helicopter Fuselages

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