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dc.rights.licenseCopyright © 2021 by the American Institute of Aeronautics and Astronautics, Inc.es
dc.contributor.authorLozano, Carloses
dc.contributor.authorPonsin, J.es
dc.date.accessioned2023-12-04T10:09:39Z-
dc.date.available2023-12-04T10:09:39Z-
dc.date.issued2021-09-25-
dc.identifier.citationAIAAJ Journal 59(12): (2021)es
dc.identifier.otherhttps://arc.aiaa.org/doi/10.2514/1.J060766es
dc.identifier.urihttp://hdl.handle.net/20.500.12666/908-
dc.descriptionCopyright © 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.sponsorshipThe 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.isoenges
dc.publisherAerospace Research Centrales
dc.subjectIncomprenssible flowes
dc.subjectAngle of attackes
dc.subjectPressure coefficientes
dc.subjectEuler equationses
dc.subjectComputational fluid dynamicses
dc.subjectFreestream mach numberes
dc.subjectAirfoil profileses
dc.subjectHomentropic flowes
dc.subjectGreen´s functiones
dc.subjectSideslip anglees
dc.titleExact inviscid drag-adjoint solution for subcritical flowses
dc.typeinfo:eu-repo/semantics/articlees
dc.identifier.doi10.2514/1.J060766-
dc.identifier.e-issn1533-385X-
dc.contributor.funderInstituto Nacional de Técnica Aeroespacial (INTA)es
dc.description.peerreviewedPeerreviewes
dc.type.hasVersioninfo:eu-repo/semantics/acceptedVersiones
dc.rights.accessRightsinfo:eu-repo/semantics/restrictedAccesses
dc.type.coarhttp://purl.org/coar/resource_type/c_6501es
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