Author Details

Shabliy, L. S.

Issue	Section	Title	File
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	(Rus)
Vol 10, No 2 (2011)	MECHANICAL ENGINEERING AND POWER ENGINEERING	Analysis of the applicability of laser stereolithography technology for the production of turbodrives	(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	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Automatization of creation vane models for CAE with PROFILER	(Rus)
Vol 11, No 3-2 (2012): Special Issue	CONFERENCE MATERIALS	Problem of multistage compressor optimization while designing perspective gas turbine engines	(Rus)
Vol 11, No 3-2 (2012): Special Issue	CONFERENCE MATERIALS	Compressor blade profile reverse-engineering: building of middle curve and symmetrical profile	(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	CFD-modeling of processes in a high-pressure oxidizer pump for the turbopump assembly of a liquid rocket engine	(Rus)
Vol 14, No 3-2 (2015): Special Issue	ISSUE WITHOUT SECTION	Application of stereolithography prototypes for gas dynamic tests	(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	(Rus)
Vol 14, No 3-2 (2015): Special Issue	ISSUE WITHOUT SECTION	Procedure of validated CFD-modeling of a two-stage screw-centrifugal pump	(Rus)
Vol 15, No 4 (2016)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Method of transient simulation of combustion processes in a low-thrust rocket engine operating on gaseous hydrogen and oxygen	(Rus)
Vol 15, No 4 (2016)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Simulation of the work process of a two-stage pump with a first-stage hydraulic drive	(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	(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	(Rus)
Vol 10, No 3-4 (2011): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Modernization of test-bench for small turbine-drives investigation	(Rus)

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