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 PDF
(Rus)
Vol 11, No 5-1 (2012): Special Issue CONFERENCE MATERIALS Reduction of circumferential variation in the final stage of IPC PDF
(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 PDF
(Rus)
Vol 11, No 5-1 (2012): Special Issue CONFERENCE MATERIALS Optimization of aircraft seven stage compressor first stages parameters PDF
(Rus)
Vol 11, No 5-1 (2012): Special Issue CONFERENCE MATERIALS Automatization of creation vane models for CAE with PROFILER PDF
(Rus)
Vol 11, No 3-1 (2012): Special Issue CONFERENCE MATERIALS Reduction of circumferential variation in the final stage of IPC PDF
(Rus)
Vol 11, No 3-2 (2012): Special Issue CONFERENCE MATERIALS Improving the high pressure compressor efficiency by optimizing the stator blades angles PDF
(Rus)
Vol 11, No 3-3 (2012): Special Issue CONFERENCE MATERIALS Approaches to parametric models of blade machines formation PDF
(Rus)
Vol 13, No 5-1 (2014): Special Issue ISSUE WITHOUT SECTION Validation of CFD-models of gas turbine engine uncooled turbines PDF
(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 PDF
(Rus)
Vol 14, No 3-2 (2015): Special Issue ISSUE WITHOUT SECTION Optimization of the workflow of multistage axial turbines with platforms PDF
(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 PDF
(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 PDF
(Rus)
Vol 21, No 1 (2022) MECHANICAL ENGINEERING Gasdynamic and strength improvement of the axial flow turbine of a helicopter gas turbine engine PDF
(Rus)
Vol 22, No 1 (2023) MECHANICAL ENGINEERING Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade PDF
(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 PDF
(Rus)

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies