Author Details

Shustov, S. A.

Issue Section Title File
Vol 12, No 2 (2013) AIRCRAFT AND SPACE ROCKET ENGINEERING Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200 PDF
(Rus)
Vol 12, No 2 (2013) AIRCRAFT AND SPACE ROCKET ENGINEERING Experimental research of wall boundary flow formation in the combustion chamber of a small gas generator with self-igniting fuel components PDF
(Rus)
Vol 12, No 2 (2013) AIRCRAFT AND SPACE ROCKET ENGINEERING Analysis of ablation process method errors for the definition of the temperature profile of high-temperature gas flows PDF
(Rus)
Vol 8, No 1 (2009) AIRCRAFT AND SPACE ROCKET ENGINEERING Approbation of the numerical model of account of viscosity impact on the flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with sliding PDF
(Rus)
Vol 8, No 1 (2009) AIRCRAFT AND SPACE ROCKET ENGINEERING Numerical model of viscosity impact on flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with velocity slip PDF
(Rus)
Vol 8, No 1 (2009) AIRCRAFT AND SPACE ROCKET ENGINEERING Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle PDF
(Rus)
Vol 10, No 3-3 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants PDF
(Rus)
Vol 10, No 3-4 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Aspects of the numerical method calculating thermogazodynamic lrest based on not perfect passing of workflows in the combustion chamber PDF
(Rus)
Vol 10, No 3-4 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Experimental research of staff LTRE with hypergolic propellant under impulse engaging conditions PDF
(Rus)
Vol 10, No 3-4 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Experimental research of thermal yet influence of staff LTRE upon the construction models of airspace devices PDF
(Rus)
Vol 21, No 1 (2022) MECHANICAL ENGINEERING On the efficiency of using the Navier-Stokes approximation in thermogasdynamic calculation of low-thrust liquid-propellant rocket engines at low Reynolds numbers PDF
(Rus)

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