| Issue |
Section |
Title |
File |
| Vol 5, No 2-2 (2006): Special Issue |
TECHNICAL SCIENCES |
Calculated study of influence of squinted form pressure side of outlet trailing edge of axial turbine vane upon projection losses in non-cooled vane row |
(Rus)
|
| Vol 7, No 3 (2008): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage |
(Rus)
|
| Vol 8, No 3-1 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Formation of a structural calculated mesh the passage blade of the axial turbine in program GAMBIT |
(Rus)
|
| Vol 8, No 3-2 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
The calculated study of fluid structure in a hub an axial aviation turbine |
(Rus)
|
| Vol 8, No 3-2 (2009): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
The story of invention and development of supercharge units of internal combustion engines |
(Rus)
|
| Vol 11, No 5-1 (2012): Special Issue |
CONFERENCE MATERIALS |
Simulation of aircraft multistage axial turbine working processes taking into account over-shroud leakage flows and blading inflows |
(Rus)
|
| Vol 11, No 5-1 (2012): Special Issue |
CONFERENCE MATERIALS |
Reduction of circumferential variation in the final stage of IPC |
(Rus)
|
| Vol 11, No 5-1 (2012): Special Issue |
CONFERENCE MATERIALS |
Approaches to modeling work of gas turbine engine`s core as a connected task |
(Rus)
|
| Vol 11, No 5-1 (2012): Special Issue |
CONFERENCE MATERIALS |
Optimization of aircraft seven stage compressor first stages parameters |
(Rus)
|
| Vol 11, No 3-2 (2012): Special Issue |
CONFERENCE MATERIALS |
Computational research of multistage turbine flow taking into account flow spatial structure and associated volumes |
(Rus)
|
| Vol 11, No 3-2 (2012): Special Issue |
CONFERENCE MATERIALS |
Selection of optimal configuration and workflow parameters of autonomous micro gas turbine plant |
(Rus)
|
| Vol 14, No 3-2 (2015): Special Issue |
ISSUE WITHOUT SECTION |
Optimization of the workflow of multistage axial turbines with platforms |
(Rus)
|
| Vol 14, No 3-2 (2015): Special Issue |
ISSUE WITHOUT SECTION |
The use of mathematical optimization means to increase the efficiency of a seven-stage axial flow compressor |
(Rus)
|
| Vol 10, No 3-3 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Determination of a rational combination of the radial turbine basic parameters with an allowance for strength, technological and other constraints |
(Rus)
|
| Vol 10, No 3-3 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Blading of radial-axial turbine wheel using Bezier curve |
(Rus)
|
| Vol 19, No 3 (2020) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Method of coordinating joint operation of air starter and auxiliary power unit and determining the gas turbine engine starting time |
(Rus)
|
| Vol 22, No 3 (2023) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Features of design calculation of compressor spool flow path of a twin-shaft gas turbine engine core on the basis of 1D and 2D models of their working process |
(Rus)
|
