Por favor, use este identificador para citar o enlazar este ítem:
http://hdl.handle.net/20.500.12666/908
Registro completo de metadatos
Campo DC | Valor | Idioma |
---|---|---|
dc.rights.license | Copyright © 2021 by the American Institute of Aeronautics and Astronautics, Inc. | es |
dc.contributor.author | Lozano, Carlos | es |
dc.contributor.author | Ponsin, J. | es |
dc.date.accessioned | 2023-12-04T10:09:39Z | - |
dc.date.available | 2023-12-04T10:09:39Z | - |
dc.date.issued | 2021-09-25 | - |
dc.identifier.citation | AIAAJ Journal 59(12): (2021) | es |
dc.identifier.other | https://arc.aiaa.org/doi/10.2514/1.J060766 | es |
dc.identifier.uri | http://hdl.handle.net/20.500.12666/908 | - |
dc.description | Copyright © 2021 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. | es |
dc.description.sponsorship | The research described in this paper has been supported by INTA and the Ministry of Defence under the grant Termofluidodinámica (IGB99001). The computations reported in the paper were carried out with DLR’s TAU Code, which is licensed to INTA through a research and development cooperation agreement, and with Stanford University’s open-source code SU2. | es |
dc.language.iso | eng | es |
dc.publisher | Aerospace Research Central | es |
dc.subject | Incomprenssible flow | es |
dc.subject | Angle of attack | es |
dc.subject | Pressure coefficient | es |
dc.subject | Euler equations | es |
dc.subject | Computational fluid dynamics | es |
dc.subject | Freestream mach number | es |
dc.subject | Airfoil profiles | es |
dc.subject | Homentropic flow | es |
dc.subject | Green´s function | es |
dc.subject | Sideslip angle | es |
dc.title | Exact inviscid drag-adjoint solution for subcritical flows | es |
dc.type | info:eu-repo/semantics/article | es |
dc.identifier.doi | 10.2514/1.J060766 | - |
dc.identifier.e-issn | 1533-385X | - |
dc.contributor.funder | Instituto Nacional de Técnica Aeroespacial (INTA) | es |
dc.description.peerreviewed | Peerreview | es |
dc.type.hasVersion | info:eu-repo/semantics/acceptedVersion | es |
dc.rights.accessRights | info:eu-repo/semantics/restrictedAccess | es |
dc.type.coar | http://purl.org/coar/resource_type/c_6501 | es |
Aparece en las colecciones: | (Aeronáutica) Artículos |
Ficheros en este ítem:
Fichero | Descripción | Tamaño | Formato | |
---|---|---|---|---|
Exact inviscid drag-adjoint solution for subcritical flows.pdf | 2,5 MB | Adobe PDF | Visualizar/Abrir |
Los ítems de Digital.INTA están protegidos por copyright, con todos los derechos reservados, a menos que se indique lo contrario.