Toward improved simulation tools for compressible turbomachinery: assessment of RBC schemes for the transonic NASA Rotor 37 benchmark case
dc.contributor.author
hal.structure.identifier | CINNELLA, Paola
|
dc.contributor.author
hal.structure.identifier | MICHEL, Bruno
|
dc.date.accessioned | 2013 |
dc.date.available | 2013 |
dc.date.issued | 2013 |
dc.date.submitted | 2013 |
dc.identifier.uri | http://hdl.handle.net/10985/7658 |
dc.description.abstract | Residual-based-compact schemes (RBC) of 2nd and 3rd-order accuracy are applied to a challenging 3D ow through a transonic compressor. The proposed schemes provide almost mesh-converged solutions in good agreement with experimental data on relatively coarse grids, which allows computational cost reductions by a factor between 2 and 4 with respect to standard solvers for a given accuracy level. |
dc.rights | Post-print |
dc.subject | Transonic compressor |
dc.subject | Residual-Based compact scheme |
dc.subject | high order |
dc.title | Toward improved simulation tools for compressible turbomachinery: assessment of RBC schemes for the transonic NASA Rotor 37 benchmark case |
dc.typdoc | Communication avec acte |
dc.localisation | Centre de Paris |
dc.subject.hal | Sciences de l'ingénieur: Mécanique: Génie mécanique |
dc.subject.hal | Sciences de l'ingénieur: Mécanique: Mécanique des fluides |
ensam.audience | Internationale |
ensam.conference.title | Congrès français de mécanique (21 ; 2013 ; Bordeaux (Gironde)). |
ensam.conference.date | 2013-08-26 |
ensam.country | France |
ensam.title.proceeding | Congrès français de mécanique (21 ; 2013 ; Bordeaux (Gironde)). |
ensam.page | 1-6 |
hal.identifier | hal-00920571 |
hal.version | 1 |
hal.submission.permitted | updateMetadata |
hal.status | accept |