Author Details

Шустов, С. А.

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	(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	(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	(Rus)
Vol 5, No 2-2 (2006): Special Issue	TECHNICAL SCIENCES	Russian aviation engines' manufacturing organizations cooperation model	(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	(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	(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	(Rus)
Vol 13, No 1 (2014)	MECHANICAL ENGINEERING AND POWER ENGINEERING	Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets	(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	(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	(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	(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	(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	(Rus)

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