Uma breve revisão das correlações para tensão de cisalhamento na parede para escoamentos hipersônicos

dc.contributor.advisorSouza, Thiago Cardoso de
dc.contributor.advisorLatteshttp://lattes.cnpq.br/2874612687747843pt_BR
dc.contributor.authorAraújo, Pedro Paulo Batista de
dc.contributor.authorID0000-0001-7850-4872pt_BR
dc.contributor.authorLatteshttp://lattes.cnpq.br/8995418183590174pt_BR
dc.contributor.referees1Maurente, André Jesus Soares
dc.contributor.referees1Latteshttp://lattes.cnpq.br/8073368791527116pt_BR
dc.contributor.referees2Meier, Rafael Becker
dc.contributor.referees2Latteshttp://lattes.cnpq.br/2236293148490315pt_BR
dc.date.accessioned2022-02-24T18:25:19Z
dc.date.available2022-02-24T18:25:19Z
dc.date.issued2022-02-11
dc.description.resumoThis paper addresses the problem of finding the appropriate correlation model for the estimation of drag force in aerospace vehicles that operate at hypersonic conditions. Here the analysis of the spatial variation of the local wall shear stress along a 6.28° ramp wall in a hypersonic flow is considered. Three cases corresponding to flows with Mach numbers corresponding to 3, 7, and 10 were analyzed. A number of correlations for the friction coefficient as proposed by Sommer and Short, Spalding and Chi, van Driest, White and Christoph, Eckert, and Meador and Smart, were applied to evaluate the wall shear using an analytical approach. The thermodynamic properties of the flow downstream of the shock wave, established at the leading edge of the ramp, were estimated using the oblique shock theory. The analytical results were compared to a reference wall shear data numerically obtained using a Reynolds-Averaged Navier-Stokes (RANS) steady-state simulation performed for the same geometry. The working fluid is air, modeled in this paper as a calorically perfect gas. For the closure of the turbulent Reynolds stresses, the k-kl-ω transition model was used. The results established a quantitative comparison between the wall shear stress curves obtained for each method, numerical and analytical. The results points out that most correlations models have low accuracy for the hypersonic flow, which is reasonable since these models were developed from experimental data extracted from supersonic flows. Despite this limitation, the analytical models which satisfactorily predicted the drag coefficient, under the conditions investigated, were the models proposed by Eckert, the model proposed by Sommer and Short for supersonic flows and the Meador and Smart model for hypersonic flow.pt_BR
dc.identifier.citationARAÚJO, Pedro Paulo Batista de. A brief review of wall shear correlations for hypersonic flows. 2022.10f. Trabalho de Conclusão de Curso (Graduação em Engenharia Mecânica) - Centro de Tecnologia, Universidade Federal do Rio Grande do Norte, Natal, 2022.pt_BR
dc.identifier.urihttps://repositorio.ufrn.br/handle/123456789/46314
dc.languageenpt_BR
dc.publisherUniversidade Federal do Rio Grande do Nortept_BR
dc.publisher.countryBrasilpt_BR
dc.publisher.departmentDepartamento de Engenharia Mecânicapt_BR
dc.publisher.initialsUFRNpt_BR
dc.publisher.programEngenharia Mecânicapt_BR
dc.subjectSkin friction dragpt_BR
dc.subjectWall shear stresspt_BR
dc.subjectCFDpt_BR
dc.subjectAnalytical correlations modelspt_BR
dc.subjectHypersonic flowpt_BR
dc.titleUma breve revisão das correlações para tensão de cisalhamento na parede para escoamentos hipersônicospt_BR
dc.title.alternativeA brief review of Wall Shear correlations for hypersonic flowspt_BR
dc.typebachelorThesispt_BR

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