| 期 |
栏目 |
标题 |
文件 |
| 卷 15, 编号 1 (2014) |
Articles |
The problem of increasing the sensitivity of local control methods for tightness products of rocket and space technology |
(Rus)
|
| 卷 12, 编号 4 (2011) |
Articles |
MATHEMATICAL MODELING OF FLOW IN THE WORKINCAVITY OF THE DISC PUMP |
(Rus)
|
| 卷 13, 编号 5 (2012) |
Articles |
DESIGN OPTIMIZATION OF THERMO-TECHNICAL SYSTEMS OPERATING IN A CLOSED CIRCUIT |
(Rus)
|
| 卷 13, 编号 5 (2012) |
Articles |
EXPERIMENTAL INVESTIGATIONS OF INCOMPRESSIBLE VISCOUS FLUID IN THE FRONT GAP BETWEEN ROTATING DISK AND FIXED BOUNDARY |
(Rus)
|
| 卷 13, 编号 5 (2012) |
Articles |
ROTATIONAL FLOWS HEAT TRANSFER IN TURBOMACHINES BASED ON TWO-LAYER MODEL OF TURBULENT BOUNDARY LAYER |
(Rus)
|
| 卷 10, 编号 3 (2009) |
Articles |
Bottom flow lines research at flow turning |
(Rus)
|
| 卷 10, 编号 3 (2009) |
Articles |
Relative characteristic thicknesses of the dynamic three-dimensional boundary layer at various laws of velocity distribution |
(Rus)
|
| 卷 22, 编号 2 (2021) |
Section 3. Technological Processes and Materials |
Conversion use of models of working processes of rocket engine turbine installations in the application to local power engineering |
(Rus)
(Eng)
|
| 卷 21, 编号 3 (2020) |
Section 2. Aviation and Space Technology |
Flow dynamics in the radial-annular cavity of turbomachines |
(Eng)
|
| 卷 20, 编号 3 (2019) |
Section 2. Aviation and Space Technology |
Determining thermal resistance in the model of the liquid circuit of spacecraft thermal control system |
(Eng)
|
| 卷 20, 编号 3 (2019) |
Section 2. Aviation and Space Technology |
Calculation of complex heat transfer in the liquid circuit of the spacecraft thermal control system based on real topology and thermophysical properties |
(Eng)
|
