Frolov, Vladimir A.

2023

• 1 Frolov V.A., Le V. Исследование коэффициента лобового сопротивления цилиндра с установленной за ним пластиной // Прикладная механика и техническая физика 2023. — Vol. 64. № 6 (382). — P. 60-67
• 2 Frolov V.A., Ha L.V. DRAG COEFFICIENT OF A CYLINDER WITH A FLAT PLATE PLACED BEHIND IT // Journal of Applied Mechanics and Technical Physics 2023. — Vol. 64. Issue 6. № 6. — P. 993-999
• 3 Khamitova E.N., Frolov V.A. ИССЛЕДОВАНИЕ АЭРОДИНАМИЧЕСКИХ ХАРАКТЕРИСТИК МОДЕЛИ ФЮЗЕЛЯЖА С РАДИОЛОКАЦИОННЫМ КОМПЛЕКСОМ В ВИДЕ ДИСКА // Journal of young scientists and specialists of the University of Samara 2023. — № 2(23). — P. 14-18
• 4 Frolov V.A. Approximate calculation of maximum lifting properties of wing-body combination // AIP Conference Proceedings. — 2023. — Vol. 2504.

2022

• 1 Frolov Vladimir Alekseevich, Le V. Reducing Drag of Cylinder by Positioning Flat Plate Back // International Conference on the Methods of Aerophysical Research. — 2022. — Pt. II. — P. 51-52

2020

• 1 Frolov V.A., Kozlova A.S. Reduction Drag of Circular Cylinder Due to Installation of Four Flat Plates // Journal of Physics: Conference Series. — 2020. — Vol. 1510. Issue 1.

2019

• 1 Frolov Vladimir Alekseevich Optimization of Lift-Curve Slope for Wing-Fuselage CombinationLondon: IntechOpen Books, 2019. 17p.
• 2 Frolov V.A. Method of calculating flow around extremely thin airfoil with slotted leading-edge slat and flap // AIP Conference Proceedings. — 2019. — Vol. 2125.

2018

• 1 Frolov V.A., Kozlova A.S. Reducing Drag of Body by Adding a Plate // MATEC Web of Conferences. — 2018. — Vol. 220.
• 2 Frolov V.A., Kozlova A.S. Influence of flat plate in front of circular cylinder on drag // AIP Conference Proceedings. — 2018. — Vol. 2027.

2017

• 1 Frolov V.A., Kozlova A.S. Reducing cylinder drag by adding a plate // AIP Conference Proceedings. — 2017. — Vol. 1893.
• 2 Frolov V. Ground effect on lift of thick wing airfoil // 2017 International Conference on Mechanical, System and Control Engineering, ICMSC 2017. — 2017. — P. 319-322

2016

• 1 Nazarov D.V., Frolov V.A., Shakhov V. G. Experimental investigation of lift for a wing-in-ground effect aircraft model // Russian Aeronautics 2016. — Vol. 59. Issue 2. — P. 206-210
• 2 Frolov V.A. Laminar separation point of flow on surface of symmetrical airfoil // AIP Conference Proceedings. — 2016. — Vol. 1770.
• 3 Frolov V.A. Laminar separation point of flow around symmetrical airfoil // 18th International Conference on the Methods of Aerophysical Research (ICMAR'2016). — 2016. — Pt. 2. — P. 64-65
• 4 Frolov V. Review Results on Wing-Body Interference // MATEC Web of Conferences. — 2016. — Vol. 75.

2015

• 1 Frolov V. Development of numerical-analytical method for calculating potential flow around 2D-body // AIP Conference Proceedings. — 2015. — Vol. 1648.
• 2 Frolov Vladimir Critical Mach number for Flow around Circular-Arc Airfoil // Applied Mechanics and Materials (AMM) 2015. — № Vol. 798. — P. 513-517
• 3 Frolov Vladimir, Redkina K.V., Chen Xinjian etc. Vortex Sheets in Flow around Airfoils with Spoilers // XVII Всероссийский семинар по управлению движением и навигации летательных аппаратов. — 2015. — P. 3-7

2014

• 1 Frolov V.A., Redkina K.V., He L. NAM application for simulation of unsteady separation flow around airfoil with spoiler // Applied Mechanics and Materials. — 2014. — Vol. 598. — P. 156-159
• 2 Frolov V.A., Dong W.M. Lift investigation of airfoil with flaps // Applied Mechanics and Materials. — 2014. — Vol. 627. — P. 89-92

2012

• 1 Chen S., Xiong F., Frolov V.A. etc. Influence of the curved ground surface on the lift of flat plate airfoil // Applied Mechanics and Materials. — 2012. — Vol. 232. — P. 261-266
• 2 Frolov V.A., Redkina K.V. Mathematical Model of a Stationary Vortex in Recirculation Area Behind the Spoiler on the Airfoi // Research and Education in Aircraft Design. READ-2012. — 2012. — P. 4-10
• 3 Frolov V.A., YANG Hao, BIT, China Lift of the Nose Droop Airfoil // Симпозиум с международным участием. Самолетостроение России. Проблемы и перспективы. — 2012. — P. 390-392

2011

• 1 Vladimir Frolov Методы расчёта несущих характеристик компоновок фюзеляж-крыло. Аналитический обзор, математические модели, расчетные и экспериментальные данные, оптимизацияGermany: LAP LAMBERT Academic Publishing GmbH & Co. KG, 2011. 148p.

2010

• 1 KLEMENTEV V.A., KURKIN E.V., LYaSKIN A.S. etc. Aerodynamic study of airfoil with rotary slat // Research and Education in Aircraft Design. — 2010. —
• 2 LYaSKIN A.S., TARASOV V.V., FROLOV V.A. etc. Internet-based technologies in research and educational applications of samara state aerospace university wind-tunnel // Research and Education in Aircraft Design. — 2010. —