Author Details

Батурин, О. В.

Issue Section Title File
Vol 5, No 2-2 (2006): Special Issue TECHNICAL SCIENCES Calculated study of influence of squinted form pressure side of outlet trailing edge of axial turbine vane upon projection losses in non-cooled vane row PDF
(Rus)
Vol 7, No 3 (2008): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage PDF
(Rus)
Vol 8, No 3-1 (2009): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Formation of a structural calculated mesh the passage blade of the axial turbine in program GAMBIT PDF
(Rus)
Vol 8, No 3-2 (2009): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING The calculated study of fluid structure in a hub an axial aviation turbine PDF
(Rus)
Vol 8, No 3-2 (2009): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING The story of invention and development of supercharge units of internal combustion engines PDF
(Rus)
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 Approaches to modeling work of gas turbine engine`s core as a connected task 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 3-2 (2012): Special Issue CONFERENCE MATERIALS Computational research of multistage turbine flow taking into account flow spatial structure and associated volumes PDF
(Rus)
Vol 11, No 3-2 (2012): Special Issue CONFERENCE MATERIALS Selection of optimal configuration and workflow parameters of autonomous micro 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 10, No 3-3 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Determination of a rational combination of the radial turbine basic parameters with an allowance for strength, technological and other constraints PDF
(Rus)
Vol 10, No 3-3 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Blading of radial-axial turbine wheel using Bezier curve 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 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)

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