| Edição |
Seção |
Título |
Arquivo |
| Volume 15, Nº 1 (2014) |
Articles |
The problem of increasing the sensitivity of local control methods for tightness products of rocket and space technology |
(Rus)
|
| Volume 12, Nº 4 (2011) |
Articles |
MATHEMATICAL MODELING OF FLOW IN THE WORKINCAVITY OF THE DISC PUMP |
(Rus)
|
| Volume 13, Nº 5 (2012) |
Articles |
DESIGN OPTIMIZATION OF THERMO-TECHNICAL SYSTEMS OPERATING IN A CLOSED CIRCUIT |
(Rus)
|
| Volume 13, Nº 5 (2012) |
Articles |
EXPERIMENTAL INVESTIGATIONS OF INCOMPRESSIBLE VISCOUS FLUID IN THE FRONT GAP BETWEEN ROTATING DISK AND FIXED BOUNDARY |
(Rus)
|
| Volume 13, Nº 5 (2012) |
Articles |
ROTATIONAL FLOWS HEAT TRANSFER IN TURBOMACHINES BASED ON TWO-LAYER MODEL OF TURBULENT BOUNDARY LAYER |
(Rus)
|
| Volume 10, Nº 3 (2009) |
Articles |
Bottom flow lines research at flow turning |
(Rus)
|
| Volume 10, Nº 3 (2009) |
Articles |
Relative characteristic thicknesses of the dynamic three-dimensional boundary layer at various laws of velocity distribution |
(Rus)
|
| Volume 22, Nº 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)
|
| Volume 21, Nº 3 (2020) |
Section 2. Aviation and Space Technology |
Flow dynamics in the radial-annular cavity of turbomachines |
(Eng)
|
| Volume 20, Nº 3 (2019) |
Section 2. Aviation and Space Technology |
Determining thermal resistance in the model of the liquid circuit of spacecraft thermal control system |
(Eng)
|
| Volume 20, Nº 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)
|
| Volume 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)
|
