Issue |
Section |
Title |
File |
Vol 1, No 2 (2002): Special Issue |
ISSUE WITHOUT SECTION |
Experience of design and lines of further improvement of gas turbine engine low-emission combustion chambers |
(Rus)
|
Vol 1, No 2 (2002): Special Issue |
ISSUE WITHOUT SECTION |
Low-emission characteristics and reliability of gas turbine engine combustion chamber and peculiarities of their provision |
(Rus)
|
Vol 12, No 3-1 (2013): Vestnik SSAU |
ISSUE WITHOUT SECTION |
Estimation of parameters of a pulse detonation engine (РDЕ) |
(Rus)
|
Vol 12, No 3-1 (2013): Vestnik SSAU |
ISSUE WITHOUT SECTION |
Homogeneous burners of two-staged combustion chambers |
(Rus)
|
Vol 12, No 3-1 (2013): Vestnik SSAU |
ISSUE WITHOUT SECTION |
Formation of microvortex gas flows in channels of a block catalyst with coplanar channels |
(Rus)
|
Vol 12, No 3-1 (2013): Vestnik SSAU |
ISSUE WITHOUT SECTION |
Effect of non-uniform compressor flow parameters on the characteristics of a gas turbine engine combustion chamber |
(Rus)
|
Vol 6, No 2 (2007): Special Issue |
TECHNICAL SCIENCES |
Developing of low emission fuel burning system in gas turbine engines |
(Rus)
|
Vol 6, No 2 (2007): Special Issue |
TECHNICAL SCIENCES |
The designing principes of afterburner system for high efficency vapour gas machine based on NK-37 engine |
(Rus)
|
Vol 8, No 3-3 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Manipulate pulsed detonation engine |
(Rus)
|
Vol 12, No 3-2 (2013): Vestnik SSAU |
ISSUE WITHOUT SECTION |
Results of primary operation of NK-37 engine low emission combustion system |
(Rus)
|
Vol 12, No 3-2 (2013): Vestnik SSAU |
ISSUE WITHOUT SECTION |
Thermal state of combustor can elements |
(Rus)
|
Vol 11, No 2 (2012) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Multisprayer low-emission combustion chamber of modern turbojet engines – N. D. Kuznetsov’s creative heritage |
(Rus)
|
Vol 11, No 3-3 (2012): Special Issue |
CONFERENCE MATERIALS |
Formation in the channels of the block catalyst the micro vortex gas flows with intense twist |
(Rus)
|
Vol 13, No 5-2 (2014): Special Issue |
ISSUE WITHOUT SECTION |
Ways of improving burners of two-staged combustion chambers |
(Rus)
|
Vol 15, No 4 (2016) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Development of an exhaust air turbine engine |
(Rus)
|
Vol 18, No 1 (2019) |
MECHANICAL ENGINEERING |
Application of additive technology of selective laser melting (SLM) in designing a low emission combustion chamber of a gas turbine plant |
(Rus)
|
Vol 19, No 1 (2020) |
MECHANICAL ENGINEERING |
New technologies implemented in the design of a low-emission combustion chamber of a gas-turbine unit |
(Rus)
|
Vol 19, No 2 (2020) |
MECHANICAL ENGINEERING |
Technology of low-emission fuel combustion and conceptual structure of the combustion chamber of a gas-turbine power plant |
(Rus)
|