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Comparison of Accuracy for Discontinuous Galerkin Schemes in the Case of a Wave and Vortex

Mathematical models and computer simulations, 2020-05, Vol.12 (3), p.445-452

Bosnyakov, I. S.

2020

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Computational Efficiency of the Ader and Runge–Kutta Schemes for the Discontinuous Galerkin Method in the Case of the 1D Hopf Equation

Mathematical models and computer simulations, 2022-02, Vol.14 (1), p.139-146

2022

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Calculation of the civil aircraft wing characteristics in critical flight modes

AIP Conference Proceedings, 2020, Vol.2288 (1)

2020

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An effective high-order numerical method for solving the Reynolds equation system in the case of civil aircraft high lift wing

AIP Conference Proceedings, 2020, Vol.2288 (1)

2020

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An Approach to Ensuring Vortex Safety of an Aircraft

Lobachevskii journal of mathematics, 2020-07, Vol.41 (7), p.1184-1189

2020

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Modeling of Aircraft Flight Through the Wake Vortex

Journal of applied mechanics and technical physics, 2019-03, Vol.60 (2), p.314-322

2019

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Features of airplane vortex wake decay in cruise flight and in land proximity

AIP Conference Proceedings, 2016, Vol.1770 (1)

2016

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Simulations of aircraft vortex wakes with high fidelity methods

AIP Conference Proceedings, 2018, Vol.2027 (1)

2018

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AIRCRAFT-CARRIER VORTEX WAKE CALCULATIONS

Nauchnyĭ vestnik MGTU GA (Online), 2016-11 (212), p.55-59

2016

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AIRCRAFT-CARRIER VORTEX WAKE CALCULATIONS

Nauchnyĭ vestnik MGTU GA (Online), 2015-01 (212), p.55-59

2015

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A High-Order Accuracy Method for Calculating the Initial Icing Stage of a Civil Aircraft’s Structural Elements

Mathematical models and computer simulations, 2024-02, Vol.16 (1), p.13-28

2024

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Numerical Simulation of Low Frequency Pulsations in the Mixing Layer of a Jet of a Full-Scale Wind Tunnel and Experiment of Modeling a Jet Actuator for Their Suppression

Mathematical models and computer simulations, 2022-02, Vol.14 (1), p.120-128

2022

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Mathematical Modeling as an Integral Part of Wind Tunnel Experimental Methodology

Mathematical models and computer simulations, 2023-02, Vol.15 (1), p.138-151

2023

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Experimental Verification of the Method and Code for Calculating Low-Frequency Fluctuations at the Jet Boundary of a Full-Scale Subsonic Looped Type Wind Tunnel

Mathematical models and computer simulations, 2024-02, Vol.16 (1), p.50-62

2024

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Numerical simulation of the flow around the wing in takeoff-landing configuration

AIP Conference Proceedings, 2018, Vol.2027 (1)

2018

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Evaluation of the Accuracy of Modern Codes by Comparing the Calculated and Experimental Data on the Example of a Problem on a Supersonic Viscous Turbulent Gas Flow Around a Tandem of Back-Forcing and Forward-Forcing Steps

Mathematical models and computer simulations, 2024-02, Vol.16 (1), p.123-155

2024

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Сравнение точности схем Галеркина с разрывными функциями на примере задач с волной и с вихрем

Matematicheskoe modelirovanie (Moscow, Russia), 2019, Vol.31 (10), p.22-34

2019

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Numerical Simulation of Supersonic Separated Flow over Inclined Backward-Facing Step Using RANS and LES Methods

Mathematical models and computer simulations, 2020-07, Vol.12 (4), p.453-463

2020

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Computational tools for supporting the testing of civil aircraft configurations in wind tunnels

Progress in aerospace sciences, 2008-02, Vol.44 (2), p.67-120

2008

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Unsteady Discontinuous Galerkin Method of a High Order of Accuracy for Modeling Turbulent Flows

Mathematical models and computer simulations, 2019, Vol.11 (1), p.22-34

2019

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TsAGI’s experience in numerical simulation of flow in cryogenic wind tunnel

AIP Conference Proceedings, 2016, Vol.1770 (1)

2016

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Efficiency of Two Approaches to Computing the Flow around an Airfoil with Flaps in the Case of Flow Separation

Computational mathematics and mathematical physics, 2019, Vol.59 (1), p.82-95

2019

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Эффективность решения одномерного уравнения Хопфа разрывным методом Галеркина схемами ADER и Рунге-Кутта

Matematicheskoe modelirovanie (Moscow, Russia), 2021-07, Vol.33 (7), p.109-120

2021

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Численное исследование низкочастотных пульсаций в слое смешения струи натурной аэродинамической трубы и опыт моделирования струйного актуатора для их подавления

Matematicheskoe modelirovanie (Moscow, Russia), 2021-07, Vol.33 (7), p.79-92

2021

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Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge

Computational mathematics and mathematical physics, 2016-06, Vol.56 (6), p.1020-1033

2016

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Comparison of Accuracy for Discontinuous Galerkin Schemes in the Case of a Wave and Vortex

Computational Efficiency of the Ader and Runge–Kutta Schemes for the Discontinuous Galerkin Method in the Case of the 1D Hopf Equation

Calculation of the civil aircraft wing characteristics in critical flight modes

An effective high-order numerical method for solving the Reynolds equation system in the case of civil aircraft high lift wing

An Approach to Ensuring Vortex Safety of an Aircraft

Modeling of Aircraft Flight Through the Wake Vortex

Features of airplane vortex wake decay in cruise flight and in land proximity

Simulations of aircraft vortex wakes with high fidelity methods

AIRCRAFT-CARRIER VORTEX WAKE CALCULATIONS

AIRCRAFT-CARRIER VORTEX WAKE CALCULATIONS

A High-Order Accuracy Method for Calculating the Initial Icing Stage of a Civil Aircraft’s Structural Elements

Numerical Simulation of Low Frequency Pulsations in the Mixing Layer of a Jet of a Full-Scale Wind Tunnel and Experiment of Modeling a Jet Actuator for Their Suppression

Mathematical Modeling as an Integral Part of Wind Tunnel Experimental Methodology

Experimental Verification of the Method and Code for Calculating Low-Frequency Fluctuations at the Jet Boundary of a Full-Scale Subsonic Looped Type Wind Tunnel

Numerical simulation of the flow around the wing in takeoff-landing configuration

Evaluation of the Accuracy of Modern Codes by Comparing the Calculated and Experimental Data on the Example of a Problem on a Supersonic Viscous Turbulent Gas Flow Around a Tandem of Back-Forcing and Forward-Forcing Steps

Сравнение точности схем Галеркина с разрывными функциями на примере задач с волной и с вихрем

Numerical Simulation of Supersonic Separated Flow over Inclined Backward-Facing Step Using RANS and LES Methods

Computational tools for supporting the testing of civil aircraft configurations in wind tunnels

Unsteady Discontinuous Galerkin Method of a High Order of Accuracy for Modeling Turbulent Flows

TsAGI’s experience in numerical simulation of flow in cryogenic wind tunnel

Efficiency of Two Approaches to Computing the Flow around an Airfoil with Flaps in the Case of Flow Separation

Эффективность решения одномерного уравнения Хопфа разрывным методом Галеркина схемами ADER и Рунге-Кутта

Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge

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