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Dynamic Ground Effect on the Aerodynamic Coefficients Using a Panel Method

2016; American Institute of Aeronautics and Astronautics; Volume: 54; Issue: 2 Linguagem: Inglês

10.2514/1.c034098

1533-3868

Pedro J. Boschetti, Gabriela Quijada, Elsa Cárdenas,

Fluid Dynamics and Vibration Analysis

No AccessEngineering NoteDynamic Ground Effect on the Aerodynamic Coefficients Using a Panel MethodPedro J. Boschetti, Gabriela M. Quijada and Elsa M. CárdenasPedro J. BoschettiUniversidad Simón Bolívar, Naiguatá 1160, Venezuela, Gabriela M. QuijadaUniversidad Simón Bolívar, Caracas 1080-A, Venezuela and Elsa M. CárdenasUniversidad Simón Bolívar, Naiguatá 1160, VenezuelaPublished Online:21 Oct 2016https://doi.org/10.2514/1.C034098SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Staufenbiel R. W. and Schlichting U. J., "Stability of Airplanes in Ground Effect," Journal of Aircraft, Vol. 25, No. 4, 1988, pp. 289–294. doi:https://doi.org/10.2514/3.45562 LinkGoogle Scholar[2] Gonzalez P., Boschetti P., Cárdenas E. and Rodriguez M., "Dynamic Ground Effect on the Longitudinal Stability of Airplanes During the Landing," AIAA Paper 2014-0384, Jan. 2014. 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Boschetti and Gabriel Leal29 December 2021Nonlinear Aerodynamic Model for Wings in Dynamic Ground EffectPedro J. Boschetti, Elsa M. Cárdenas, Pedro J. González and Alejandro Merkl2 June 2020 | Journal of Aircraft, Vol. 57, No. 6Dependence of the Flight-path on the Aerodynamic Characteristics of Rectangular Wings due to Dynamic Ground EffectAlejandro Merkl, Pedro J. Boschetti and Elsa M. Cardenas6 January 2019Nonlinear Models for Representing Aerodynamic Coefficients of a Wing in Ground EffectPedro J. Boschetti and Elsa M. Cárdenas7 January 2018 What's Popular Volume 54, Number 2March 2017Special Section on Cranked Arrow Wing Aerodynamics Project International II/F-16XL CrossmarkInformationCopyright © 2016 by Pedro J. Boschetti. 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 ISSN 0021-8669 (print) or 1533-3868 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsAerospace SciencesAircraft Dynamic ModesComputational Fluid DynamicsFlight DynamicsFlight MechanicsFlow RegimesFluid DynamicsNumerical AnalysisVortex Dynamics KeywordsAerodynamic CharacteristicsLift CoefficientAspect RatioVortex FilamentsIncompressible FlowFlight VehicleFlight Control SystemNumerical ModelingWing in Ground EffectMean Aerodynamic ChordPDF Received22 June 2016Accepted5 August 2016Published online21 October 2016