Toward improved simulation tools for compressible turbomachinery: assessment of Residual-Based Compact schemes for the transonic compressor NASA Rotor 37
dc.contributor.author
hal.structure.identifier | CINNELLA, Paola
|
dc.contributor.author | MICHEL, Bruno |
dc.date.accessioned | 2015 |
dc.date.available | 2015 |
dc.date.issued | 2014 |
dc.date.submitted | 2015 |
dc.identifier.issn | 1061-8562 |
dc.identifier.uri | http://hdl.handle.net/10985/10078 |
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 achieving a given accuracy level with computational cost reductions by a factor between 2 and 4 with respect to standard solvers. |
dc.description.sponsorship | FP7- Projet IDIHOM |
dc.language.iso | en |
dc.publisher | Taylor & Francis |
dc.rights | Post-print |
dc.title | Toward improved simulation tools for compressible turbomachinery: assessment of Residual-Based Compact schemes for the transonic compressor NASA Rotor 37 |
dc.identifier.doi | 10.1080/10618562.2014.886686 |
dc.typdoc | Article dans une revue avec comité de lecture |
dc.localisation | Centre de Paris |
dc.subject.hal | Mathématique: Analyse numérique |
dc.subject.hal | Sciences de l'ingénieur: Mécanique: Mécanique des fluides |
ensam.audience | Internationale |
ensam.page | 31-40 |
ensam.journal | International Journal of Computational Fluid Dynamics |
ensam.volume | 28 |
hal.identifier | hal-01202618 |
hal.version | 1 |
hal.submission.permitted | updateMetadata |
hal.status | accept |
dc.identifier.eissn | 1029-0257 |