Author Details

Popov, G. M.

Issue	Section	Title	File
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Simulation of aircraft multistage axial turbine working processes taking into account over-shroud leakage flows and blading inflows	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Reduction of circumferential variation in the final stage of IPC	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Investigation of effects of multistage compressor final stage blading shape on compressor performance and flow pattern	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Optimization of aircraft seven stage compressor first stages parameters	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Automatization of creation vane models for CAE with PROFILER	(Rus)
Vol 11, No 3-1 (2012): Special Issue	CONFERENCE MATERIALS	Reduction of circumferential variation in the final stage of IPC	(Rus)
Vol 11, No 3-2 (2012): Special Issue	CONFERENCE MATERIALS	Improving the high pressure compressor efficiency by optimizing the stator blades angles	(Rus)
Vol 11, No 3-3 (2012): Special Issue	CONFERENCE MATERIALS	Approaches to parametric models of blade machines formation	(Rus)
Vol 13, No 5-1 (2014): Special Issue	ISSUE WITHOUT SECTION	Validation of CFD-models of gas turbine engine uncooled turbines	(Rus)
Vol 13, No 5-1 (2014): Special Issue	ISSUE WITHOUT SECTION	Peculiarities of modeling the work process in a low-pressure compressor of a gas turbine plant	(Rus)
Vol 14, No 3-2 (2015): Special Issue	ISSUE WITHOUT SECTION	Optimization of the workflow of multistage axial turbines with platforms	(Rus)
Vol 14, No 3-2 (2015): Special Issue	ISSUE WITHOUT SECTION	The use of mathematical optimization means to increase the efficiency of a seven-stage axial flow compressor	(Rus)
Vol 19, No 3 (2020)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Method of coordinating joint operation of air starter and auxiliary power unit and determining the gas turbine engine starting time	(Rus)
Vol 21, No 1 (2022)	MECHANICAL ENGINEERING	Gasdynamic and strength improvement of the axial flow turbine of a helicopter gas turbine engine	(Rus)
Vol 22, No 1 (2023)	MECHANICAL ENGINEERING	Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade	(Rus)
Vol 22, No 3 (2023)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Features of design calculation of compressor spool flow path of a twin-shaft gas turbine engine core on the basis of 1D and 2D models of their working process	(Rus)
Vol 23, No 3 (2024)	MECHANICAL ENGINEERING	Gas dynamic optimization of the work process of a single-stage cooled axial turbine with an inside baffle	(Rus)

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