Suscripción a Biblioteca: Guest

SIMULATION OF PERIODIC VORTICAL STRUCTURES IN THE AIRFOIL WAKE

Volumen 45, Edición 3-4, 2014, pp. 273-292
DOI: 10.1615/TsAGISciJ.2014011965
Get accessGet access

SINOPSIS

Parametrical calculations of an unsteady flow around a NACA 0012 airfoil at a fixed Reynolds number of 40,000 are performed using several multi-block overlapping grids of different scales and densities, which cover settlement areas of various extents, including the near and far wakes. The solutions found by Menter's shear stress transport model, the Spalart−Allmaras vortex viscosity transport model, and the method of vortical domains, are compared with available estimated and experimental data. Verification of the two-dimensional model is performed by comparison of the numerical predictions for a cross flow over a thick plate with Igarashi's experimental data.

CITADO POR
  1. Isaev S. A., Miau J.-J., Sudakov A. G., Usachov A. E., Analysis of extremal lift behavior of a semicircular airfoil in a turbulent airflow at a near-zero angle of attack, Technical Physics Letters, 41, 8, 2015. Crossref

  2. Zhang G.Q., Ji L.C., Investigation of two degrees of freedom on vortex-induced vibration under the wake interference of an oscillating airfoil, Acta Astronautica, 133, 2017. Crossref

  3. Isaev S. A., Baranov P. A., Zhukova Yu. V., Kalinin E. I., Miau J. J., Verification of the Shear-Stress Transfer Model and its Modifications in the Calculation of a Turbulent Flow Around a Semicircular Airfoil with a Zero Angle of Attack, Journal of Engineering Physics and Thermophysics, 89, 1, 2016. Crossref

  4. Isaev Sergey, Baranov Paul, Popov Igor, Sudakov Alexander, Usachov Alexander, Guvernyuk Sergey, Sinyavin Alexei, Chylunin Alexei, Mazo Alexander, Kalinin Eugeny, Ensuring safe descend of reusable rocket stages – Numerical simulation and experiments on subsonic turbulent air flow around a semi-circular cylinder at zero angle of attack and moderate Reynolds number, Acta Astronautica, 150, 2018. Crossref

  5. Isaev S. A., Experience of application of SST-model-2003 with correction on streamline curvature according to Rodi-Leshziner-Isaev approach for (U)RANS calculations of separated and vortex sub- and supersonic flows, 2027, 2018. Crossref

  6. Isaev Sergey, Baranov Paul, Popov Igor, Sudakov Alexander, Usachov Alexander, Guvernyuk Sergey, Sinyavin Alexei, Chulyunin Alexei, Mazo Alexander, Demidov Dennis, Dekterev Alexander, Gavrilov Andrey, Shebelev Alexander, Numerical simulation and experiments on turbulent air flow around the semi-circular profile at zero angle of attack and moderate Reynolds number, Computers & Fluids, 188, 2019. Crossref

  7. Isaev Sergey, Nikushchenko Dmitry, Sudakov Alexandr, Tryaskin Nikita, Egorova Ann, Iunakov Leonid, Usachov Alexandr, Kharchenko Valery, Standard and Modified SST Models with the Consideration of the Streamline Curvature for Separated Flow Calculation in a Narrow Channel with a Conical Dimple on the Heated Wall, Energies, 14, 16, 2021. Crossref

  8. Исаев Сергей Александрович, Isaev Sergey Aleksandrovich, Мяу Дж Дж, Miau J J, Никущенко Дмитрий Владимирович, Nikushchenko Dmitry Vladimirovich, Судаков Александр Григорьевич, Sudakov Alexandr Grigorievitch, Усачов Александр Евгеньевич, Usachov Alexandr Evgen'evich, Моделирование влияния сдвига ветра на снижение лобового сопротивления энергоэффективного высотного сооружения с использованием дросселирующего эффекта, Математическое моделирование, 33, 7, 2021. Crossref

  9. Isaev S. A., Miau J.-J., Nikushchenko D. V., Sudakov A. G., Usachov A. E., Modeling the Effect of Wind Shear on Reducing the Drag of an Energy-Efficient High-Rise Structure Using the Throttle Effect, Mathematical Models and Computer Simulations, 14, 1, 2022. Crossref

  10. Isaev Sergey, Baranov Paul, Popov Igor, Sudakov Alexander, Usachov Alexander, Improvement of aerodynamic characteristics of a thick airfoil with a vortex cell in sub- and transonic flow, Acta Astronautica, 132, 2017. Crossref

Último edicion

KIRILL IVANOVICH SYPALO−50TH ANNIVERSARY NUMERICAL STUDY OF THE DISTURBANCES GENERATED BY MICROJETS IN A SUPERSONIC FLAT-PLATE BOUNDARY LAYER Andrei Valerievich Novikov, Alexander Vitalyevich Fedorov, Ivan Vladimirovich Egorov, Anton Olegovich Obraz, Nikolay Nikolaevich Semenov ANALYSIS OF THE MOVING DETONATION INTERACTION WITH TURBULENT BOUNDARY LAYERS IN A DUCT ON THE BASIS OF NUMERICAL SIMULATION Vladimir Anatolievich Sabelnikov, Vladimir Viktorovich Vlasenko, Sergey Sergeyevich Molev EXPERIMENTAL STUDY OF COUNTERFLOW BLOWING IN HIGH-SPEED FLOW THROUGH AN ASYMMETRIC SLOT IN THE LEADING EDGE OF A SHARP WEDGE Eduard Borisovich Vasilevskii, Ivan Valeryevich Ezhov, Pavel Vladimirovich Chuvakhov ASYMPTOTIC SOLUTIONS TO HYPERSONIC BOUNDARY LAYER EQUATIONS ON A FLAT WING WITH A POINT OF INFLECTION ON THE LEADING EDGE Georgiy Nikolaevich Dudin, Aleksey Vyacheslavovich Ledovskiy WAVE MODEL OF ORGANIZED STRUCTURES IN A TURBULENT BOUNDARY LAYER ON A PLATE WITH ZERO LONGITUDINAL PRESSURE GRADIENT Vladimir Alekseevich Zharov, Igor Ivanovich Lipatov, Rami Salah Saber Selim NUMERICAL SIMULATION OF THE FLOW AROUND LANDSCAPE FRAGMENTS AND SOLUTION VERIFICATION Viktor Viktorovich Vyshinsky, Koang T'in' Zoan POLYNOMIAL REPRESENTATION OF THERMODYNAMIC PROPERTIES OF COMBINED FUEL SYSTEMS IN RAMJET SIMULATION MODELS Timur Romanovich Zuev, Mikhail Semenovich Tararyshkin A MODEL TEST METHODOLOGY FOR THE INVESTIGATION OF AN ELASTICALLY SCALED MAIN ROTOR Maxim Andreyevich Ledyankin , Sergey Anatolyevich Mikhailov, Dmitry Valeryevich Nedel'ko, Timur Arturovich Agliullin INDEX, VOLUME 51, 2020
Portal Digitalde Biblioteca Digital eLibros Revistas Referencias y Libros de Ponencias Colecciones Precios y Políticas de Suscripcione Begell House Contáctenos Language English 中文 Русский Português German French Spain