Popov, Grigoriy M.

2025

• 1 Popov G., Zubanov V., Melnikov S. etc. Prediction of the two stage turbine cavities thermal state with calculating unsteady processes of hot gas inflow // Journal of Physics: Conference Series. — 2025. — Vol. 3041. Issue 1. № 1.

2024

• 1 Popov G.M., Zubanov V.M., Goryachkin E.S. etc. Improving the Accuracy of Performance Calculation for Multistage Axial Turbines of Aircraft Engines Using Three-Dimensional Numerical Modeling // Russian Aeronautics 2024. — Vol. 67. Issue 1. № 1. — P. 96-102
• 2 Popov G.M., Zubanov V.M., Baturin O.V. etc. Linked multidisciplinary optimisation of a twin-shaft turbine of a promising turboshaft engine // Journal of Physics: Conference Series. — 2024. — Vol. 2784. Issue 1. № 1.
• 3 Matveev V.N., Popov G.M., Goriachkin E.S. etc. Algorithm of Forming the Appearance of the Flow Path of Turbomachinery of Two-Shaft Aircraft Engine Core // Proceedings of the 19th International Conference on Software Technologies, ICSOFT 2024. — 2024. — P. 223-228
• 4 Liu X., Baturin O., Popov G. Research on Multifactor Analysis Method for Thermodynamic Calculation of Turbofan Engine // ACM International Conference Proceeding Series. — 2024. — P. 171-176
• 5 Popov G.M., Melnikov S.A., Goriachkin E.S. etc. Selection of the Required Cooling Air Flow Through the Blades of the Axial Turbine at the Initial Design Stage // 2024 10th Asia Conference on Mechanical Engineering and Aerospace Engineering, MEAE 2024. — 2024. — P. 61-65
• 6 Popov G.M., Zubanov V.M., Melnikov S.A. etc. Numerical Simulation of the Thermal State of the Turbine Nozzle Guide Vane of a Modern Gas Turbine Engine // 2024 10th Asia Conference on Mechanical Engineering and Aerospace Engineering, MEAE 2024. — 2024. — P. 275-282
• 7 Liu X., Baturin O., Popov G. etc. A New Method of Conceptual Design of the Flow Part of a Gas Turbine Engine // 2024 10th Asia Conference on Mechanical Engineering and Aerospace Engineering, MEAE 2024. — 2024. — P. 339-343
• 8 Popov G.M., Matveev V.N., Zubanov V.M. etc. Improved Algorithm for Design Thermodynamic Calculation of Axial Turbomachinery Parameters of Core Engine of a Single-shaft Turboprop Engine // 2nd Asian Aerospace and Astronautics Conference, AAAC 2024. — 2024. — P. 231-237
• 9 Goriachkin E.S., Popov G.M., Gataullina E.D. etc. Complex Aerodynamic Design of a Gas Turbine Multistage Axial Compressor Using Multilevel Mathematical Models // 2024 10th Asia Conference on Mechanical Engineering and Aerospace Engineering, MEAE 2024. — 2024. — P. 100-107
• 10 Liu X., Baturin O., Popov G. etc. Research on Thermodynamics Comprehensive Analysis Method Considering the Life Cycle of Turbofan Engine // 2nd Asian Aerospace and Astronautics Conference, AAAC 2024. — 2024. — P. 184-189

2023

• 1 Popov G., Zubanov V., Goriachkin E. etc. Optimization of the Working Process of a Two-Stage HPT of a Modern GTE for Civil Aviation // International Journal of Mechanical Engineering and Robotics Research 2023. — Vol. 12. Issue 1. № 1. — P. 48-56
• 2 Popov G., Zubanov V., Goriachkin E. etc. Verification of a Numerical Model of a Two-Stage HPT of a Modern GTE for Civil Aviation // International Journal of Mechanical Engineering and Robotics Research 2023. — Vol. 12. Issue 2. № 2. — P. 78-83
• 3 Lyu S., Baturin O.V., Melnikov S.A. etc. Research on Thermal State Optimization of High Pressure Turbine 1st Stage Rotor Blade // Международная научно-техническая конференция имени Н.Д. Кузнецова "Перспективы развития двигателестроения". — 2023. — Vol. 2. — P. 112-113
• 4 Matveev V.N., Goriachkin E.S., Popov G.M. etc. The features of design calculation stages of parameters of flow path of cascade compressor of twin shaft gas turbine engine core on base of 1d and 2d dimensional models of their working process // Proceedings of the International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2023. — Vol. 1. — P. 225-233
• 5 Zubanov V.M., Popov G.M., Melnikov S.A. etc. Improving the thermal condition of the high-pressure turbine blade // Proceedings of the International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2023. — Vol. 1. — P. 234-242

2022

• 1 Volkov A., Zubanov V., Matveev V. etc. Rational Settings of a Numerical Model to Simulate the Working Process of an Axial-Film-Cooled Turbine Blade // International Journal of Mechanical Engineering and Robotics Research 2022. — Vol. 11. Issue 12. № 12. — P. 901-907
• 2 Popov G., Egorov I., Goriachkin E. etc. Optimization Method of the Multistage Axial Compressors Using CFD Simulation // International Journal of Computational Methods 2022. —
• 3 Popov G.M., Goryachkin E.S., Baturin O.V. etc. Aerodynamic and strength improvement of the axial turbine of a helicopter GTE // GPPS Xi'an21. — 2022. —
• 4 Popov Grigoriy Mikhaylovich, Mikheev M.G. , Baturin O.V. etc. Aerodynamic Improvement Of The 16-Stage Axial Compressor // GPPS Xi’an21. — 2022. —
• 5 Baturin O.V., Paúl Nicolalde, Popov G.M. etc. Calculating the parameters of a gas turbine engine taking into account the uncertainty of the initial data // GPPS Xi’an21 . — 2022. —
• 6 Popov G.M., Volkov A.A., Baturin O.V. etc. Numerical Model of the Axial Turbine Blade Cooling Process // GPPS Xi'an21. — 2022. —

2021

• 1 Popov G., Miheev M., Zubanov V. etc. Improvement of the aerodynamic parameters of a 16-stage axial compressor for industrial gas turbine power unit // AIAA Propulsion and Energy Forum, 2021. — 2021. —
• 2 Kudryashov Ivan Aleksandrovich, Popov G.M., Goryachkin E.S. Исследование влияния многорежимности газотурбинного двигателя на характеристики осевого компрессора // 20th International Conference “Aviation and Cosmonautics” (AviaSpace2021). 22-26 November 2021. Moscow. Abstracts. — 2021. — P. 120-121
• 3 Popov G.M., Baturin O.V., Goriachkin E.S. etc. Multidisciplinary optimization of a helicopter GTE Turbine // AIAA Propulsion and Energy Forum, 2021. — 2021. —
• 4 Baturin O., Popov G., Nicolalde P. etc. IDENTIFICATION of the MATHEMATICAL MODEL of A GAS TURBINE ENGINE TAKING into ACCOUNT the UNCERTAINTY of the INITIAL DATA // Proceedings of ASME 2021 Gas Turbine India Conference, GTINDIA 2021. — 2021. —
• 5 Prokofiev A.B., Baturin O.V., Popov G.M. etc. Improving the performance of a two-stage centrifugal pump by optimizing its flowpath // AIP Conference Proceedings. — 2021. — Vol. 2351.
• 6 Popov G.M., Novikova Y.D., Goryachkin E.S. etc. Design and Development of a Pneumatic Braking Device for Testing the Gas Turbine Plant // Russian Aeronautics 2021. — Vol. 64. Issue 1. — P. 52-60
• 7 Popov G.M., Zubanov V.M., Novikova Y.D. etc. A method for checking the possibility of joint work of the auxiliary power unit and the starter // Journal of Physics: Conference Series. — 2021. — Vol. 1891. Issue 1.
• 8 Popov G., Goriachkin E., Egorov I. etc. Improvement of aerodynamic and strength characteristics of a multi-shaft axial turbine of a turboshaft engine // Proceedings of the ASME Turbo Expo. — 2021. — Vol. 2D-2021.
• 9 Kharitonova Anna Alekseevna, Zubanov V.M., Scherban A.I. etc. Численное исследование характеристик соплового аппарата осевой турбины с учетом различной геометрии входной области // 20th International Conference “Aviation and Cosmonautics” (AviaSpace2021). 22-26 November 2021. Moscow. Abstracts.. — 2021. — P. 158-159
• 10 Popov G., Miheev M., Vorobyev A. etc. COMPREHENSIVE PERFORMANCE IMPROVEMENT for A 16-STAGE AXIAL COMPRESSOR // Proceedings of the ASME Turbo Expo. — 2021. — Vol. 2A-2021.
• 11 Popov G.M., Volkov A.A., Kudryashov I.A. etc. Search for Rational Settings of a Numerical Model of for Studying Film Cooling in Axial Turbines // 2021 International Scientific and Technical Engine Conference (EC). — 2021. — P. 1-5
• 12 Nepomnyaschiy V.O., Popov G.M., Miheev M.G. etc. Analysis of 16-Stage Compressor Working Process for an Industrial Gas Turbine Uint // 2021 International Scientific and Technical Engine Conference (EC). — 2021. — P. 1-5
• 13 Popov G.M., Goriachkin E.S., Baturin O.V. etc. Joint aerodynamics and strength optimization of a single-stage uncooled turbine with a shroud platform // 2021 International Scientific and Technical Engine Conference (EC). — 2021. — P. 1-8

2020

• 1 Popov G.M., Baturin O.V., Zubanov V.M. etc. The method of matching the joint work of the auxiliary power unit and turbostarter and determining the start time of the gas turbine engine // AIAA Propulsion and Energy 2020 Forum. — 2020. — P. 1-10
• 2 Popov Grigoriy Mikhaylovich, Zubanov V.M., Matveev V.N. etc. Метод согласования совместной работы воздушного стартера и вспомогательной силовой установки // Вестник ПНИПУ. Аэрокосмическая техника 2020. — № 63. — P. 5-13
• 3 Zubanov V., Popov G., Egorov I. etc. Method for determining the applicability of an air turbine for operation in a gas turbine engine launch system // SIMULTECH 2020 - Proceedings of the 10th International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2020. — P. 147-154
• 4 Zubanov V.M., Popov G.M., Volkov A.A. etc. Optimization of an air turbostarter of a launch system for gas turbine engine // AIAA Propulsion and Energy 2020 Forum. — 2020. — P. 1-9
• 5 Popov G., Goriachkin E., Baturin O. etc. Optimization of the workflow of multistage axial compressors using modern gas dynamics computing systems // Proceedings of the ASME Turbo Expo. — 2020. — Vol. 2D-2020.
• 6 Popov G., Zubanov V., Baturin O. etc. Optimization of an air turbo starter considering its joint work with an auxiliary power unit // Proceedings of the ASME Turbo Expo. — 2020. — Vol. 2C-2020.
• 7 Popov G., Matveev V., Zubanov V. etc. Improving the start-up parameters of a gas turbine engine by adaptation the air turbine starter // IOP Conference Series: Materials Science and Engineering. — 2020. — Vol. 904. Issue 1.
• 8 Goriachkin E., Popov G., Baturin O. etc. Method for improving multi-stage compressor parameters using the IOSO optimizer // SIMULTECH 2020 - Proceedings of the 10th International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2020. — P. 163-170
• 9 Popov G.M., Baturin O.V., Goriachkin E.S. etc. Optimization algorithm for axial multistage compressor workflow // AIAA Propulsion and Energy 2020 Forum. — 2020. — P. 1-11
• 10 Popov G., Baturin O., Goriachkin E. etc. Axial compressor optimization method // IOP Conference Series: Materials Science and Engineering. — 2020. — Vol. 904. Issue 1.
• 11 Popov G., Baturin O., Zubanov V. etc. Optimization of a single-stage air starter turbine // SIMULTECH 2020 - Proceedings of the 10th International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2020. — P. 155-162

2019

• 1 Egorov I., Volkov A., Popov G. etc. Multi-level model of the centrifugal compressor workflow for its effective optimization // IOP Conference Series: Materials Science and Engineering. — 2019. — Vol. 643. Issue 1.
• 2 Popov G.M., Egorov I., Dmitriev D. etc. Complex gas dynamic optimization of a three spool axial compressor of an industrial gas turbine engine // ASME 2019 Gas Turbine India Conference, GTINDIA 2019. — 2019. — Vol. 1.
• 3 Baturin O., Kolmakova D., Popov G. etc. Reducing the hydraulic resistance in the inlet device of the gas turbine unit // SIMULTECH 2019 - Proceedings of the 9th International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2019. — P. 88-99
• 4 Popov G., Volkov A., Goriachkin E. etc. NLH calculation of the influence the inlet nonuniformity on the fan parameters // IOP Conference Series: Materials Science and Engineering. — 2019. — Vol. 643. Issue 1.
• 5 Baturin O., Krivtsov A., Kolmakova D. etc. Estimation of the hydraulic losses in the work shaft of a gas turbine engine of a gas compressor unit under various operating conditions // Proceedings of the ASME Turbo Expo. — 2019. — Vol. 3.
• 6 Marchukov E., Egorov I., Popov G. etc. Creating a multi-level model of a centrifugal compressor for a digital analogue of the gas turbine engine // IOP Conference Series: Materials Science and Engineering. — 2019. — Vol. 604. Issue 1.
• 7 Marchukov E., Egorov I., Popov G. etc. Optimization of a three spool axial compressor to increase the efficiency of a gas turbine engine // IOP Conference Series: Materials Science and Engineering. — 2019. — Vol. 604. Issue 1.
• 8 Popov G.M., Matveev V.N., Zubanov V.M. etc. Selection of parameters for numerical models of the working process of axial uncooled turbines intended perform optimization and verification calculations // AIAA Propulsion and Energy Forum and Exposition, 2019. — 2019. —
• 9 Baturin O., Kolmakova D., Krivcov A. etc. Estimation of the hydraulic losses in the work shaft of a gas turbine engine of a gas compressor unit under various operating conditions // AIAA Propulsion and Energy Forum and Exposition, 2019. — 2019. —
• 10 Marchukov E., Egorov I., Popov G. etc. Increase of efficiency of axial uncooled turbine by optimization of its blades shape using cfd and optimization software // AIAA Propulsion and Energy Forum and Exposition, 2019. — 2019. —
• 11 Baturin O.V., Kolmakova D.A., Krivtsov A.V. etc. Estimation of the hydraulic losses in the inlet shaft of a land-based gas turbine // ASME 2019 Gas Turbine India Conference, GTINDIA 2019. — 2019. — Vol. 2.
• 12 Popov G.M., Egorov I., Marchukov E. etc. The concept of a multi-level optimization model of the centrifugal compressor workflow // ASME 2019 Gas Turbine India Conference, GTINDIA 2019. — 2019. — Vol. 1.
• 13 Popov G., Baturin O., Volkov A. etc. The influence of the level of the flow path blockage at the inlet on the fan characteristics // SIMULTECH 2019 - Proceedings of the 9th International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2019. — P. 247-254
• 14 Marchukov E., Egorov I., Baturin O. etc. Multi-level "Learnable" Model of the workflow in the centrifugal compressor stage // SIMULTECH 2019 - Proceedings of the 9th International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2019. — P. 100-110
• 15 Popov G., Goriachkin E., Novikova Y. etc. Evaluation of the impact of stall phenomena on the characteristics of the fan using the NLH method // Proceedings - 2019 21st International Conference "Complex Systems: Control and Modeling Problems", CSCMP 2019. — 2019. — Vol. 2019-September. — P. 570-575
• 16 Marchukov E., Egorov I., Popov G. etc. Concept Development and Approbation of a Multi-Level Model of the Centrifugal Compressor Workflow for Quick Obtaining the Reliable Characteristics in Optimization Tasks // Proceedings - 2019 21st International Conference "Complex Systems: Control and Modeling Problems", CSCMP 2019. — 2019. — Vol. 2019-September. — P. 514-518
• 17 Popov G., Goriachkin E., Egorov I. etc. Multidisciplinary optimization of compressor stage with different parameterization methods // AIAA Propulsion and Energy Forum and Exposition, 2019. — 2019. —
• 18 Egorov I., Marchukov E., Volkov A. etc. The concept of obtaining reliable compressor characteristics based on a multilevel mathematical model with a two-stage identification // AIAA Propulsion and Energy Forum and Exposition, 2019. — 2019. —
• 19 Popov G.M., Baturin O.V., Novikova Y.D. etc. Estimation of the influence of the inlet nonuniformity on the performance of a fan of a turbofan engine // ASME 2019 Gas Turbine India Conference, GTINDIA 2019. — 2019. — Vol. 1.

2018

• 1 Egorov I., Buyukli T., Popov G. etc. Experimental Compressor Multidisciplinary Optimization Using Different Parameterization Schemes // MATEC Web of Conferences. — 2018. — Vol. 220.
• 2 Zubanov V., Volkov A., Matveev V. etc. Optimization of fuel two-stage screw centrifugal pump of rocket powerful turbopump unit // Proceedings of the ASME Turbo Expo. — 2018. — Vol. 2B-2018.
• 3 Matveev V., Baturin O., Popov G. The Optimization of Four-Stage Low Pressure Turbine with Outlet Guide Vane // IOP Conference Series: Materials Science and Engineering. — 2018. — Vol. 302. Issue 1.
• 4 Kolmakova D., Popov G. Gas-Dynamic Methods to Reduce Gas Flow Nonuniformity from the Annular Frames of Gas Turbine Engines // IOP Conference Series: Materials Science and Engineering. — 2018. — Vol. 302. Issue 1.
• 5 Ermakov A., Popov G., Kolmakova D. etc. Strategy for reduction of the negative effects of circumferential flow irregularity in axial compressor // SIMULTECH 2018 - Proceedings of 8th International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2018. — P. 144-150
• 6 Popov G., Matveev V., Baturin O. etc. Selection of Parameters for Blade-To-blade Finite-volume Mesh for CFD Simulation of Axial Turbines // MATEC Web of Conferences. — 2018. — Vol. 220.
• 7 Popov G., Matveev V., Baturin O. etc. Selection of Parameters for 3D Finite-volume Mesh for CFD Simulation of Axial Turbines // MATEC Web of Conferences. — 2018. — Vol. 220.
• 8 Baturin O., Popov G., Kolmakova D. etc. Optimization of Powerful Two-stage Screw Centrifugal Pump // MATEC Web of Conferences. — 2018. — Vol. 220.
• 9 Popov G., Matveev V., Baturin O. etc. Estimation of the effect of 3d grid parameters on the simulation of the working process of axial turbines // SIMULTECH 2018 - Proceedings of 8th International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2018. — P. 371-377
• 10 Baturin O., Kolmakova D., Popov G. etc. Improving the characteristics of two-stage fuel pump by optimizing the blades geometry // SIMULTECH 2018 - Proceedings of 8th International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2018. — P. 357-364

2017

• 1 Baturin O., Tkachenko A., Krupenich I. etc. Identifying the approach to significantly improve the performance of NK-36ST gas turbine power plant // Proceedings of the ASME Turbo Expo. — 2017. — Vol. 3.
• 2 Matveev V., Novikova Y., Popov G. etc. Design and operational development a pneumatic braking system for a gas-turbine units test bench // Proceedings of the ASME Turbo Expo. — 2017. — Vol. 2B-2017.
• 3 Popov G.M., Novikova Y.D., Goryachkin E.S. etc. Using of low-pressure compressor to design the concept of the air brake system // AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting. — 2017. —
• 4 Popov G.M., Goriachkin E.S., Novikova Y.D. Многокритериальная оптимизация рабочего процесса осевого компрессора газотурбинного двигателя с учетом многорежимности его работы // Известия Самарского научного центра РАН 2017. — Vol. 19. № 1. — P. 98-106
• 5 Popov G.M., Baturin O.V., Goriachkin E.S. etc. Оптимизация рабочего процесса осевой неохлаждаемой турбины с использованием решателя 3D уравнений Навье-Стокса // Известия Самарского научного центра РАН 2017. — Vol. 19. № 1. — P. 107-115
• 6 Baturin O.V., Gorshkov A.Yu., Popov G.M. etc. Выбор модели для оценки профильных потерь в лопаточном венце с помощью методов математической статистики // Известия Самарского научного центра РАН 2017. — Vol. 19. № 1 (2). — P. 319-324
• 7 Marchukov E., Egorov I., Popov G. etc. Optimization of blades stagger angles of the three-spool axial compressor to improve of efficiency of the gas turbine engine // 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017. — 2017. —
• 8 Popov G.M., Baturin O.V., Goriachkin E.S. etc. Increasing the efficiency of the axial low pressure compressor in three operation modes by optimizing the shape of its blades // Journal of Physics: Conference Series. — 2017. — Vol. 803. Issue 1.
• 9 Novikova Y., Popov G., Goriachkin E. etc. The process of gas-dynamic design of pneumatic braking system using the baseline compressor // IOP Conference Series: Materials Science and Engineering. — 2017. — Vol. 232. Issue 1.
• 10 Marchukov E.Yu., Egorov I., Popov G. etc. Multidisciplinary optimization of the working process of uncooled axial turbine according to efficiency and strength criteria // Proceedings of the ASME Turbo Expo. — 2017. — Vol. 2C-2017.
• 11 Marchukov E., Egorov I., Popov G. etc. Improving of the working process of axial compressors of gas turbine engines by using an optimization method // IOP Conference Series: Materials Science and Engineering. — 2017. — Vol. 232. Issue 1.
• 12 Baturin O.V., Popov G.M., Kolmakova D.A. etc. The best model for the calculation of profile losses in the axial turbine // Journal of Physics: Conference Series. — 2017. — Vol. 803. Issue 1.
• 13 Baturin O.V., Popov G.M., Goryachkin E.S. etc. Optimization of the working process of the axial compressor according to the criterion of efficiency // Journal of Physics: Conference Series. — 2017. — Vol. 803. Issue 1.
• 14 Matveev V.N., Baturin O.V., Kolmakova D.A. etc. Gas dynamic improvement of the axial compressor design for reduction of the flow non-uniformity level // Journal of Physics: Conference Series. — 2017. — Vol. 803. Issue 1.
• 15 Baturin O.V., Popov G.M., Kolmakova D.A. etc. Strength and gas dynamic methods of development of the axial turbine turbocharger // Journal of Physics: Conference Series. — 2017. — Vol. 803. Issue 1.
• 16 Baturin O., Popov G., Novikova J. etc. Strength and gas dynamic methods of development of axial turbine turbocharger // 2017 International Conference on Mechanical, System and Control Engineering, ICMSC 2017. — 2017. — P. 44-47
• 17 Matveev V., Baturin O., Kolmakova D. etc. Reduction of gas flow nonuniformity in gas turbine engines by means of gas-dynamic methods // IOP Conference Series: Materials Science and Engineering. — 2017. — Vol. 232. Issue 1.

2016

• 1 Y. D. Novikova, G. M. Popov Design of the Air Brake for the GTE Test Bench by Using Methods of Computational Gas Dynamics // The Fourth International Academic Conference for Graduates. — 2016. — Pt. 2. — P. 40-43
• 2 E. S. Goriachkin, G. M. Popov Multicriteria Optimization of Axial Low Pressure Compressor Workflow // The Fourth International Academic Conference for Graduates. — 2016. — Pt. 2. — P. 50-55
• 3 Popov G., Goriachkin E., Kolmakova D. etc. Multicriteria optimization of axial low pressure compressor of gas turbine power plant // Proceedings of the ASME Turbo Expo. — 2016. — Vol. 2C-2016.
• 4 Kolmakova D., Popov G., Shklovets A. etc. Rational design of gas turbine engine compressor to provide the required dynamic strength level of rotor blades // Proceedings of the ASME Turbo Expo. — 2016. — Vol. 7A-2016.
• 5 Baturin O., Kolmakova D., Gorshkov A. etc. Generation of the equations for the profile losses calculation in blade row of axial turbines in design analysis // Proceedings of the ASME Turbo Expo. — 2016. — Vol. 2C-2016.

2015

• 1 Matveev V. N., Baturin O. V., Popov G. M. etc. ОПТИМИЗАЦИЯ РАБОЧЕГО ПРОЦЕССА МНОГОСТУПЕНЧАТЫХ ОСЕВЫХ ТУРБИН С БАНДАЖНЫМИ ПОЛКАМИ // Vestnik of the Samara State Aerospace University 2015. — № Том 14, № 3, ч. 2. — P. 271-283
• 2 Kolmakova D., Popov G. Methods of improving the axial compressor flow passage to reduce the flow circumferential nonuniformity // ASME 2015 Gas Turbine India Conference, GTINDIA 2015. — 2015. —
• 3 Popov G.M., Novikova Y.D., Goriachkin E.S. Gas dynamic designing of pneumatic braking system for gas turbine engine test bench // ASME 2015 Gas Turbine India Conference, GTINDIA 2015. — 2015. —
• 4 Matveev V.N., Popov G.M., Baturin O.V. etc. Workflow optimization of multistage axial turbine // 51st AIAA/SAE/ASEE Joint Propulsion Conference. — 2015. —
• 5 Popov G.M., Kolmakova D., Shklovets A.O. Angular arrangement optimization of the support racks of gas turbine engine to reduce the circumferential unevenness of gas flow // SIMULTECH 2015 - 5th International Conference on Simulation and Modeling Methodologies, Technologies and Applications, Proceedings. — 2015. — P. 383-388
• 6 Matveev V.N., Popov G.M., Baturin O.V. etc. Workflow optimization of multistage axial turbine // 51st AIAA/SAE/ASEE Joint Propulsion Conference. — 2015. —
• 7 Baturin O., Kolmakova D., Gorshkov A. etc. Selection of models to assess the profile losses in blade rows using the methods of mathematical statistics // ASME 2015 Gas Turbine India Conference, GTINDIA 2015. — 2015. —
• 8 Popov G., Kolmakova D., Shklovets A. etc. Optimization of the axial compressor flow passage to reduce the circumferential distortion // IOP Conference Series: Materials Science and Engineering. — 2015. — Vol. 90. Issue 1.
• 9 Baturin O.V., Popov G.M., Goryachkin E.S. etc. Application of 3D navier-stokes equations and mathematical optimization techniques to improve the efficiency of seven-stage axial compressor // SIMULTECH 2015 - 5th International Conference on Simulation and Modeling Methodologies, Technologies and Applications, Proceedings. — 2015. — P. 227-232
• 10 Kolmakova D., Popov G., Baturin O. etc. The quantification of impact of geometrical and operational parameters uncertainty on the numerical simulation results of axial turbine working process // Proceedings of the ASME Turbo Expo. — 2015. — Vol. 2B.
• 11 Goryachkin E., Baturin O., Popov G. etc. Three-stage low pressure compressor modernization by means of optimization methods // Proceedings of the ASME Turbo Expo. — 2015. — Vol. 2C.

2014

• 1 E.S. Gorachkin, G.M. Popov, Y.D. Smirnova Идентификация математических моделей турбин газотурбинных двигателей // Вестник Двигателестроения 2014. — № № 2. — P. 34-41
• 2 Ermakov A.I., Shklovets A.O., Popov G.M. etc. Investigation of the effect of the gas turbine compressor supports on gas flow circumferential nonuniformity // Research Journal of Applied Sciences 2014. — Vol. 9. Issue 10. — P. 684-690
• 3 Popov G.M., Goryachkin E.S., Baturin O.V. etc. Development of recommendations on building of the lightweight calculation mathematical models of the axial turbines of gas turbine engines // International Journal of Engineering and Technology 2014. — Vol. 6. Issue 5. — P. 2236-2243
• 4 Matveev V.N., Baturin O.V., Popov G.M. etc. Seven-stage axial compressor optimization // Engineering Optimization IV - Proceedings of the 4th International Conference on Engineering Optimization, ENGOPT 2014. — 2014. — P. 821-826
• 5 Matveev V.N., Baturin O.V., Popov G.M. etc. The results of gas dynamic and strength improvement of turbocharger TK-32 axial turbine // SIMULTECH 2014 - Proceedings of the 4th International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2014. — Vol. 2014-January. — P. 595-600
• 6 Kolmakova D.A., Baturin O.V., Popov G.M. Knowledge lack impact assessment of the source date on numerical simulation results of operational process in axial flow turbine blade row // ARPN Journal of Engineering and Applied sciences 2014. — Vol. 9. Issue 12. — P. 2880-2889
• 7 Kolmakova D., Baturin O., Popov G. Effect of manufacturing tolerances on the turbine blades // In Proceedings of the ASME 2014 Gas Turbine India Conference GTINDIA2014. — 2014. —
• 8 Popov G.M., Shklovets A.O., Ermakov A.I. etc. Methods to reduce the resonant stresses level of gas turbine engines compressor rotor wheels // SIMULTECH 2014 - Proceedings of the 4th International Conference on Simulation and Modeling Methodologies, Technologies and Applications. — 2014. — Vol. 2014-January. — P. 619-624
• 9 Popov G.M., Baturin O.V., Kolmakova D.A. etc. Improvement results of TK-32 turbocompressor turbine with gas-dynamics and strength CAE-systems // International Journal of Engineering and Technology 2014. — Vol. 6. Issue 5. — P. 2297-2303
• 10 Matveev V.N., Popov G.M., Goryachkin E.S. etc. Effect of accounting of air bleed from the flow passage of the multi-stage axial low pressure compressor on its design performances // Research Journal of Applied Sciences 2014. — Vol. 9. Issue 11. — P. 784-788
• 11 Kolmakova D., Popov G., Shklovets A. etc. Techniques and methods to improve the dynamic strength of gas turbine engines compressor rotor wheels // ASME 2014 Gas Turbine India Conference, GTINDIA 2014. — 2014. —

2013

• 1 MATVEEV V.N., BATURIN O.V., POPOV G.M. etc. Efficiency impruvement of a multistagae compressor by optimization stagger angles of blade rows // 4th CEAS conference. — 2013. — P. 148-148
• 2 MATVEEV V.N., BATURIN O.V., POPOV G.M. etc. Efficiency improvement of a multistage compressorby optimization stagger angles of blade rows // Proceedings of the 4:thCEAS Conference in Linkoping 2013. — P. 761-768