Please use this identifier to cite or link to this item: http://hdl.handle.net/20.500.12666/898
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dc.rights.licenseCopyright © 2018 by Instituto Nacional de Técnica Aeroespacial (INTA)es
dc.contributor.authorBardera, Rafaeles
dc.contributor.authorGarcía Magariño, A.es
dc.contributor.authorRodríguez Sevillano, A.es
dc.contributor.authorBarcala Montejano, M. Á.es
dc.date.accessioned2023-11-28T10:54:31Z-
dc.date.available2023-11-28T10:54:31Z-
dc.date.issued2019-01-11-
dc.identifier.citationJournal of Aircraft 56(3): 1005-1013(2019)es
dc.identifier.issn0021-8669-
dc.identifier.otherhttps://arc.aiaa.org/doi/10.2514/1.C035188es
dc.identifier.urihttp://hdl.handle.net/20.500.12666/898-
dc.descriptionCopyright © 2018 by Instituto Nacional de Técnica Aeroespacial (INTA). Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3868 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.es
dc.description.abstractThe aircraft takeoff maneuver for onboard operations is the most critical aspect of maritime performance. In the last decades, several improvements have been made to reduce the number of accidents. One of them is the ski-jump ramp, a modern takeoff system that allows the maneuver to be performed more safely and using less runway distance. Thus, a new in-depth aerodynamic study of the ramp is required. A wind-tunnel test campaign was developed to study the disturbances caused by the ski-jump ramp over the flight deck and the influence on an aircraft carrier performance. Smoke visualizations over the ramp revealed a detached unsteady recirculation bubble at the ramp and a turbulent flow over the flight deck. Velocity measurements were carried out by means of particle image velocimetry. The influence of these disturbances was evaluated for the takeoff performance of the AV-8B Harrier II. The results proved the importance of taking into account these disturbance effects and provided a detailed characterization of the flow over the carrier deck, resulting in establishment of a useful background for future studies on aircraft–ship interference.es
dc.description.sponsorshipThis investigation was funded by the Spanish Ministry of Defense under the INTA program “Termofluidodinámica”.es
dc.language.isoenges
dc.publisherAerospace Research Centrales
dc.subjectAerodynamic performancees
dc.subjectAerodynamicses
dc.subjectBoundary layerses
dc.subjectComputational fluid dynamicses
dc.subjectFlow measurementses
dc.subjectFlow regimeses
dc.subjectFluid dynamicses
dc.subjectNumerical analysises
dc.subjectNumerical interpolationes
dc.subjectTurbulencees
dc.subjectVelocimetryes
dc.subjectVortex dynamicses
dc.subjectWind tunnelses
dc.titleAerodynamic Flow Effects on Aircraft Carrier Takeoff Performancees
dc.typeinfo:eu-repo/semantics/articlees
dc.identifier.doihttps://doi.org/10.2514/1.C035188-
dc.identifier.e-issn1533-3868-
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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