Author Details

Shakhov, V. G.

Issue	Section	Title	File
Vol 7, No 2 (2008)	CONTROL, COMPUTER SCIENCE AND INFORMATION SCIENCE	Multi-time-step scheme in the vorticity splitting method applied to the simulation of the wake behind the flat plate	(Rus)
Vol 8, No 4 (2009)	MECHANICAL ENGINEERING AND POWER ENGINEERING	Applying Lagrange’s approach to solving a one-dimensional problem of wave propagation in gas in linear formulation	(Rus)
Vol 10, No 2 (2011)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Application of Cebeci’s method for solving time-dependent problems of the incompressible boundary layer	(Rus)
Vol 11, No 5-1 (2012): Special Issue	CONFERENCE MATERIALS	Gas-discharge generation of near-wall flows	(Rus)
Vol 11, No 4 (2012)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Peculiarities of solving three-dimensional problems of flow about a launch vehicle with large nose fairings using the ANSYS FLUENT software	(Rus)
Vol 16, No 3 (2017)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Influence of turbulence models on calculated values of aircraft aerodynamic properties	(Rus)
Vol 1, No 1 (2002)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Approximate solution of a laminar boundary layer on moving surfaces without use of integral relations	(Rus)
Vol 2, No 1 (2003)	AIRCRAFT AND SPACE ROCKET ENGINEERING	COMPUTING VORTICITY DIFFUSION WITH A MODIFIED "DONOR-ACCEPTOR" SCHEME AND THE INTEGRATION OF THE SCHEME INTO THE "VORTEX-IN-CELL" METHOD	(Rus)