Author Details

Шаблий, Л. С., Самарский государственный аэрокосмический университет имени академика С.П. Королёва (национальный исследовательский университет), Russian Federation

Issue Section Title File
Vol 8, No 3-2 (2009): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Electronic model of turbine drive flow for its direct optimization PDF
(Rus)
Vol 10, No 2 (2011) MECHANICAL ENGINEERING AND POWER ENGINEERING Estimation of the adequacy of electronic flow model and efficiency characteristic of small centripetal turbine drive PDF
(Rus)
Vol 10, No 2 (2011) MECHANICAL ENGINEERING AND POWER ENGINEERING Analysis of the applicability of laser stereolithography technology for the production of turbodrives 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 Automatization of creation vane models for CAE with PROFILER PDF
(Rus)
Vol 11, No 3-2 (2012): Special Issue CONFERENCE MATERIALS Problem of multistage compressor optimization while designing perspective gas turbine engines PDF
(Rus)
Vol 11, No 3-2 (2012): Special Issue CONFERENCE MATERIALS Compressor blade profile reverse-engineering: building of middle curve and symmetrical profile 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 CFD-modeling of processes in a high-pressure oxidizer pump for the turbopump assembly of a liquid rocket engine PDF
(Rus)
Vol 14, No 3-2 (2015): Special Issue ISSUE WITHOUT SECTION Application of stereolithography prototypes for gas dynamic tests PDF
(Rus)
Vol 14, No 3-2 (2015): Special Issue ISSUE WITHOUT SECTION Methods of modeling the work process of hydrogen screw-centrifugal pumps using ANSYS CFD PDF
(Rus)
Vol 14, No 3-2 (2015): Special Issue ISSUE WITHOUT SECTION Procedure of validated CFD-modeling of a two-stage screw-centrifugal pump PDF
(Rus)
Vol 10, No 3-3 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Automatization of creation vane 3D-model in Ansys TurboGrid with geometry data in traditional view 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 3-4 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Modernization of test-bench for small turbine-drives investigation PDF
(Rus)

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