| 期 |
栏目 |
标题 |
文件 |
| 卷 14, 编号 4 (2013) |
Articles |
HEAT TRANSFER IN THE CAVITY OF A GAS TURBINE LIQUID ROCKET ENGINE |
(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 24, 编号 2 (2023) |
Section 2. Aviation and Space Technology |
To the method of calculation of the main characteristics of promising booster electric pump units of liquid processor engines |
(Rus)
|
| 卷 23, 编号 2 (2022) |
Section 2. Aviation and Space Technology |
Dynamics of the flow in the sections of the elements of the supply path of the turbopump unit of the LRE |
(Rus)
|
| 卷 23, 编号 3 (2022) |
Section 2. Aviation and Space Technology |
Local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines |
(Rus)
|
| 卷 21, 编号 3 (2020) |
Section 2. Aviation and Space Technology |
Heat transfer in the centrifugal force field for gas turbines elements |
(Eng)
|
| 卷 20, 编号 2 (2019) |
Section 2. Aviation and Space Technology |
The method of the disk friction determining of low mass flow centrifugal pumps |
(Eng)
|
| 卷 21, 编号 2 (2020) |
Section 2. Aviation and Space Technology |
The method of the disk friction determining of low mass flow centrifugal pumps |
(Eng)
|
