| Issue |
Section |
Title |
File |
| Vol 5, No 2-2 (2006): Special Issue |
TECHNICAL SCIENCES |
Method of regressive analysis of experimental and calculation characteristics of centripetal microturbines nozzle apparatus |
(Rus)
|
| 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 |
Uniform and equidistant ways of structured computation grigd creation for CFD problems |
(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 story of invention and development of supercharge units of internal combustion engines |
(Rus)
|
| Vol 10, No 2 (2011) |
MECHANICAL ENGINEERING AND POWER ENGINEERING |
Estimation of the adequacy of electronic flow model and efficiency characteristic of small centripetal turbine drive |
(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 |
Optimization of aircraft seven stage compressor first stages parameters |
(Rus)
|
| Vol 11, No 3-2 (2012): Special Issue |
CONFERENCE MATERIALS |
Key focus areas of samara state aerospace university research and education center of gasdynamic research |
(Rus)
|
| Vol 13, No 5-1 (2014): Special Issue |
ISSUE WITHOUT SECTION |
Validation of CFD-models of gas turbine engine uncooled turbines |
(Rus)
|
| Vol 13, No 5-1 (2014): Special Issue |
ISSUE WITHOUT SECTION |
Peculiarities of modeling the work process in a low-pressure compressor of a 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 |
Application of stereolithography prototypes for gas dynamic tests |
(Rus)
|
| Vol 15, No 4 (2016) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Simulation of the work process of a two-stage pump with a first-stage hydraulic drive |
(Rus)
|
| Vol 10, No 3-4 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Modernization of test-bench for small turbine-drives investigation |
(Rus)
|
| Vol 21, No 1 (2022) |
MECHANICAL ENGINEERING |
Gasdynamic and strength improvement of the axial flow turbine of a helicopter gas turbine engine |
(Rus)
|
| Vol 22, No 1 (2023) |
MECHANICAL ENGINEERING |
Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade |
(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)
|
