Produção Nacional
Revisado por pares
Lift Prediction Including Stall, Using Vortex Lattice Method with Kirchhoff-Based Correction
2017; American Institute of Aeronautics and Astronautics; Volume: 55; Issue: 2 Linguagem: Inglês
10.2514/1.c034451
ISSN1533-3868
AutoresCarlos R. dos Santos, Flávio D. Marques,
Tópico(s)Aerodynamics and Fluid Dynamics Research
ResumoNo AccessEngineering NoteLift Prediction Including Stall, Using Vortex Lattice Method with Kirchhoff-Based CorrectionCarlos R. dos Santos and Flávio D. MarquesCarlos R. dos SantosUniversity of São Paulo, 13566-590 São Carlos SP, Brazil*Graduate Student, São Carlos School of Engineering; (Corresponding Author).Search for more papers by this author and Flávio D. MarquesUniversity of São Paulo, 13566-590 São Carlos SP, Brazil†Associate Professor, São Carlos School of Engineering; .Search for more papers by this authorPublished Online:6 Sep 2017https://doi.org/10.2514/1.C034451SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Harper C. W. and Maki R. L., “A Review of the Stall Characteristics of Swept Wings,” NASA Ames Research Center NASA-TN-D-2373, Mountain View, CA, 1964. Google Scholar[2] Petrilli J., Paul R., Gopalarathnam A. and Frink N. 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TopicsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsAircraft DesignAircraft Operations and TechnologyAircraft Wing DesignComputational Fluid DynamicsFinite Element MethodFlow RegimesFluid DynamicsTurbulenceTurbulence ModelsVortex DynamicsWing ConfigurationsWing Planforms KeywordsVortex Lattice MethodLift CoefficientAspect RatioFreestream VelocityVortex RingsInfluence CoefficientsRectangular WingSweep AngleAirfoil ProfilesWing RootAcknowledgmentsThe authors acknowledge the financial support of the São Paulo State Research Foundation FAPESP (grant nos. 2014/21166-7 and 2016/24522-4) and the Brazilian Research Agency CNPq (grant no. 305700/2013-8).PDF Received2 March 2017Accepted11 July 2017Published online6 September 2017
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