Computational Simulation of Airfoils Stall Aerodynamics at Low Reynolds Numbers

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dc.cclicenceCC-BY-NCen
dc.contributor.authorSereez, Mohameden
dc.contributor.authorAbramov, Nikolayen
dc.contributor.authorGoman, M. (Mikhail G.)en
dc.date.accessioned2017-04-10T12:39:48Z
dc.date.available2017-04-10T12:39:48Z
dc.date.issued2016-07-19
dc.description.abstractExperimental results for aerodynamic static hysteresis at stall conditions obtained in the TsAGI's T-124 low-turbulence wind tunnel for NACA0018 are presented and analysed. Computational predictions of aerodynamic static hysteresis are made using the OpenFOAM simulations considering di erent grids, turbulence models and solvers. Comparisons of compu- tational simulation results with experimental wind tunnel data are made for 2D NACA0018 and NACA0012 airfoils at low Reynolds numbers Re = (0.3-1.0) millions. The properties of the proposed phenomenological bifurca- tion model for simulation of aerodynamic loads at the existence of static hysteresis are discussed.en
dc.funderN/Aen
dc.identifier.citationSereez, M., Abramov, N. and Goman, M. (2015) Computational Simulation of Airfoils Stall Aerodynamics at Low Reynolds Numbers. Royal Aeronautical Society, Applied Aerodynamics Conferenceen
dc.identifier.isbn1857683714
dc.identifier.urihttp://hdl.handle.net/2086/14049
dc.language.isoenen
dc.projectidN/Aen
dc.publisherRoyal Aeronautical Societyen
dc.researchgroupEngineering and Physical Sciences Institute (EPsi)
dc.subjectAerodynamicsen
dc.subjectCFDen
dc.subjectStatic hysteresisen
dc.subjectbifurcationsen
dc.titleComputational Simulation of Airfoils Stall Aerodynamics at Low Reynolds Numbersen
dc.typeConferenceen

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