Author Details

Matveev, V. N.

Issue	Section	Title	File
Vol 7, No 3 (2008): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Uniform and equidistant ways of structured computation grigd creation for CFD problems	(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	(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	(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	(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	Optimization of aircraft seven stage compressor first stages parameters	(Rus)
Vol 11, No 3-2 (2012): Special Issue	CONFERENCE MATERIALS	Key focus areas of samara state aerospace university research and education center of gasdynamic research	(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	Application of stereolithography prototypes for gas dynamic tests	(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 3-4 (2011): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Modernization of test-bench for small turbine-drives investigation	(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)

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