| Issue |
Section |
Title |
File |
| Vol 12, No 3-1 (2013): Vestnik SSAU |
ISSUE WITHOUT SECTION |
Correlation and regression model for the assessment of circular non-uniformity of the gas temperature field at the outlet of small gas turbine engine combustion chambers |
(Rus)
|
| Vol 12, No 3-1 (2013): Vestnik SSAU |
ISSUE WITHOUT SECTION |
Mathematical model for calculating radial non-uniformity of the gas temperature field at the exit of small gas turbine engine combustion chambers |
(Rus)
|
| Vol 12, No 3-1 (2013): Vestnik SSAU |
ISSUE WITHOUT SECTION |
Development of an algorithm of design calculation of a combustion chamber for microturbine electric power plants |
(Rus)
|
| Vol 12, No 3-1 (2013): Vestnik SSAU |
ISSUE WITHOUT SECTION |
Influence of the turbine ignition, flame tube suspension and nozzles on the combustion chamber characteristics |
(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 12, No 3-1 (2013): Vestnik SSAU |
ISSUE WITHOUT SECTION |
Formation of carcinogenic PAHs (polyaromatic hydrocarbons) in the turbulent diffusive flame |
(Rus)
|
| Vol 8, No 3-1 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Modeling of the heat exchange processes |
(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 |
Combined calculation of gas generators of small GTE in package ANSYS CFX |
(Rus)
|
| Vol 11, No 5-2 (2012): Special Issue |
CONFERENCE MATERIALS |
Problems and solutions of using computer technologies in designing of combustion chambers GTE |
(Rus)
|
| Vol 14, No 2 (2015) |
MECHANICAL ENGINEERING AND POWER ENGINEERING |
Determination of thermal state and modification of the flame tube cooling system with the help of three-dimensional modeling methods |
(Rus)
|
| Vol 10, No 5 (2011) |
ISSUE WITHOUT SECTION |
Modeling of propane combustion processes in case of converting a GTE combustion chamber to gaseous fuel |
(Rus)
|
| Vol 10, No 5 (2011) |
ISSUE WITHOUT SECTION |
Simulation of aerodynamic structure of the flow in the combustion chamber of a small-size gas turbine engine with the help of CAE–systems |
(Rus)
|
| Vol 10, No 5 (2011) |
ISSUE WITHOUT SECTION |
Construction of detailed kinetic mechanisms of forming for five ring PAH and their reduction for use in modern CAE systems |
(Rus)
|
| Vol 15, No 4 (2016) |
MECHANICAL ENGINEERING AND POWER ENGINEERING |
Dependence of methane laminar flame propagation speed on the pressure and initial temperature |
(Rus)
|
| Vol 18, No 1 (2019) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Development of blend composition of aviation kerosene surrogate for the simulation of workflow of gas turbine engine combustion chamber |
(Rus)
|
| Vol 20, No 2 (2021) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Calculation of flow characteristics of liquid fuel supplied through pressure jet atomizers of small-sized gas turbine engines |
(Rus)
|
| Vol 21, No 3 (2022) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Kinetic model and kerosene surrogate for calculating gas turbine engine emission of carcinogenic hydrocarbons |
(Rus)
|
