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Please use this identifier to cite or link to this item: http://acervodigital.unesp.br/handle/11449/32861
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dc.contributor.authorGomes, FAA-
dc.contributor.authorSilva, JBC-
dc.contributor.authorDiniz, A. J.-
dc.date.accessioned2014-05-20T15:21:45Z-
dc.date.accessioned2016-10-25T17:55:16Z-
dc.date.available2014-05-20T15:21:45Z-
dc.date.available2016-10-25T17:55:16Z-
dc.date.issued2006-01-01-
dc.identifierhttp://dx.doi.org/10.2514/1.15495-
dc.identifier.citationJournal of Spacecraft and Rockets. Reston: Amer Inst Aeronaut Astronaut, v. 43, n. 1, p. 236-239, 2006.-
dc.identifier.issn0022-4650-
dc.identifier.urihttp://hdl.handle.net/11449/32861-
dc.identifier.urihttp://acervodigital.unesp.br/handle/11449/32861-
dc.format.extent236-239-
dc.language.isoeng-
dc.publisherAmer Inst Aeronaut Astronaut-
dc.sourceWeb of Science-
dc.titleFormulation of the ablation thermal problem in a unified formen
dc.typeoutro-
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)-
dc.description.affiliationState Univ São Paulo, Dept Mech Engn, Fac Engn, BR-15385000 São Paulo, Brazil-
dc.description.affiliationUnespState Univ São Paulo, Dept Mech Engn, Fac Engn, BR-15385000 São Paulo, Brazil-
dc.identifier.doi10.2514/1.15495-
dc.identifier.wosWOS:000235380100029-
dc.rights.accessRightsAcesso restrito-
dc.relation.ispartofJournal of Spacecraft and Rockets-
Appears in Collections:Artigos, TCCs, Teses e Dissertações da Unesp

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