| Issue |
Section |
Title |
File |
| Vol 14, No 4 (2013) |
Articles |
HEAT TRANSFER IN THE CAVITY OF A GAS TURBINE LIQUID ROCKET ENGINE |
(Rus)
|
| Vol 13, No 5 (2012) |
Articles |
DESIGN OPTIMIZATION OF THERMO-TECHNICAL SYSTEMS OPERATING IN A CLOSED CIRCUIT |
(Rus)
|
| Vol 13, No 5 (2012) |
Articles |
EXPERIMENTAL INVESTIGATIONS OF INCOMPRESSIBLE VISCOUS FLUID IN THE FRONT GAP BETWEEN ROTATING DISK AND FIXED BOUNDARY |
(Rus)
|
| Vol 13, No 5 (2012) |
Articles |
ROTATIONAL FLOWS HEAT TRANSFER IN TURBOMACHINES BASED ON TWO-LAYER MODEL OF TURBULENT BOUNDARY LAYER |
(Rus)
|
| Vol 10, No 3 (2009) |
Articles |
Bottom flow lines research at flow turning |
(Rus)
|
| Vol 10, No 3 (2009) |
Articles |
Relative characteristic thicknesses of the dynamic three-dimensional boundary layer at various laws of velocity distribution |
(Rus)
|
| Vol 24, No 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)
|
| Vol 23, No 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)
|
| Vol 23, No 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)
|
| Vol 21, No 3 (2020) |
Section 2. Aviation and Space Technology |
Heat transfer in the centrifugal force field for gas turbines elements |
(Eng)
|
| Vol 20, No 2 (2019) |
Section 2. Aviation and Space Technology |
The method of the disk friction determining of low mass flow centrifugal pumps |
(Eng)
|
| Vol 21, No 2 (2020) |
Section 2. Aviation and Space Technology |
The method of the disk friction determining of low mass flow centrifugal pumps |
(Eng)
|
| Vol 25, No 1 (2024) |
Section 2. Aviation and Space Technology |
Power engineering of the tangential supply device of the microturbine of the thermal control system of a promising spacecraft |
(Rus)
(Eng)
|
