Nonlinear Rolling Motion of Triform Finned Missiles

Morote, J.; Liaño, Gabriel; Jiménez-Varona, José

Publicación:
Nonlinear Rolling Motion of Triform Finned Missiles

dc.contributor.author	Morote, J.
dc.contributor.author	Liaño, Gabriel
dc.contributor.author	Jiménez-Varona, José
dc.date.accessioned	2026-02-19T07:01:26Z
dc.date.available	2026-02-19T07:01:26Z
dc.date.issued	2017-01-31
dc.description.abstract	A theoretical investigation of the rolling motion of triform configurations at high angles of attack is presented. A nonlinear aerodynamic flow model, derived from strip and slender body theories, is used to predict the aerodynamic roll coefficients of triform tailed missiles at high angles of attack. The flow model predictions are compared to the estimates of a panel-based code and a computational fluid dynamics code at two Mach numbers.
dc.description.peerreviewed	Peerreview
dc.identifier.citation	Journal of Spacecraft and Rockets 54(2)
dc.identifier.doi	10.2514/1.A33764
dc.identifier.e-issn	1533-6794
dc.identifier.issn	0022-4650
dc.identifier.other	https://arc.aiaa.org/doi/10.2514/1.A33764
dc.identifier.uri	https://hdl.handle.net/20.500.12666/1731
dc.language.iso	eng
dc.publisher	AIAA - American Institute of Aeronautics and Astronautics
dc.rights.accessRights	info:eu-repo/semantics/restrictedAccess
dc.rights.license	Copyright © 2016 by the American Institute of Aeronautics and Astronautics
dc.subject	Missiles
dc.subject	Angle of Attack
dc.subject	Aeroprediction
dc.subject	Slender body theory
dc.subject	Computational fluid dynamics code
dc.subject	Aerodynamic flows
dc.subject	Fluent
dc.subject	Vortex shedding
dc.subject	Turbulence models
dc.subject	Subsonic velocity
dc.title	Nonlinear Rolling Motion of Triform Finned Missiles
dc.type	info:eu-repo/semantics/article
dc.type.coar	http://purl.org/coar/resource_type/c_2df8fbb1
dc.type.hasVersion	info:eu-repo/semantics/publishedVersion
dspace.entity.type	Publication
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relation.isAuthorOfPublication.latestForDiscovery	661680d7-756f-4160-99c5-d25e52f5db9f