Compressibility Correction to Kutta–Joukowski and Maskell Formulas Using Vortex-Force Theory
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No AccessTechnical NotesCompressibility Correction to Kutta–Joukowski and Maskell Formulas Using Vortex-Force TheoryCamille Fournis, Didier Bailly Renato TognacciniCamille FournisONERA–The French Aerospace Lab, 92190 Meudon, France*Ph.D. Student, Aerodynamics, Aeroelasticity Acoustics Department; .Search for more papers by this author, BaillyONERA–The France†Research Engineer, author TognacciniUniversity of Naples Federico II, 80125 Naples, Italy‡Associate Professor, Dipartimento di Ingegneria Industriale; . Senior Member AIAA.Search authorPublished Online:31 Oct 2020https://doi.org/10.2514/1.J059710SectionsRead Now ToolsAdd favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Kutta W. M., “Auftriebskräfte in Strömenden Flüssigkeiten,” Illustrierte Aeronautische Mitteilungen, Vol. 6, No. 133, 1902, pp. 133–135. 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Scholar[18] Unified Foundations Lift External Flows, Springer, 117. https://doi.org/10.1007/978-981-10-6223-0 Scholar[19] Fournis Reference Point Invariant Aerodynamic Breakdown Scitech 2020 Forum, 2020-1996, 2020. https://doi.org/10.2514/6.2020-1996 Scholar[20] Ostieri “Vorticity 54, 4, 2016, 1198–1208. https://doi.org/10.2514/1.J054363 Scholar[21] “Aircraft Transonic 1933–1944. https://doi.org/10.2514/1.C034288 Scholar[22] Russo Z. 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Sforza P. “Some Remarks Wakes Jets,” 12, 1968, 2454–2456. https://doi.org/10.2514/3.5025 Scholar[31] Kuo Baldwin “Diffusion Decay Turbulent Elliptic Wakes,” 1966, 1566–1572. https://doi.org/10.2514/3.3737 Scholar[32] Bradshaw P., “Compressible Shear Layers,” 1977, 33–52. https://doi.org/10.1146/annurev.fl.09.010177.000341 Scholar Previous article FiguresReferencesRelatedDetailsCited byWave FlowsMauro Minervino Tognaccini19 January 2023Invariant Extending Classical Theories FlowsCamille Tognaccini2 May 2022 | 60, 9Wave drag prediction using vector two-dimensional steady transonic flowsCamille Fournis20 June 2022Drag Fields: M6 WingPierce Hart Sven Schmitz13 December 2021 5An Overview Research Activities Related BreakdownDidier Bailly, Ilias Petropoulos, Christelle Wervaecke, Michaël Méheut, Olivier Atinault Camille Fournis28 July 2021An invariant vortex-force theory related classical far-field analyses Tognaccini28 2021Application Field Schmitz28 What's Popular Volume 59, Number 2February CrossmarkInformationCopyright © The Authors. Published American Institute Aeronautics Astronautics, Inc., permission. All requests copying permission reprint should be submitted CCC at www.copyright.com; employ eISSN 1533-385X initiate your request. See also Rights Permissions www.aiaa.org/randp. TopicsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsComputational DynamicsConservation Mass EquationsEquations DynamicsFlow RegimesFluid DynamicsFluid PropertiesTurbulenceTurbulence ModelsVortex DynamicsWind Tunnels KeywordsVortex SheetCompressibilityKutta TheoremIn FlowsReynolds Averaged Navier StokesCFDLift CoefficientCompressibility EffectGas ConstantSpalart Allmaras Turbulence ModelAcknowledgmentPart research was supported Direction Générale de l’Armement scholarship.PDF Received16 April 2020Accepted4 October 2020Published online31
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ژورنال
عنوان ژورنال: AIAA Journal
سال: 2021
ISSN: ['0001-1452', '1533-385X', '1081-0102']
DOI: https://doi.org/10.2514/1.j059710