| Issue |
Section |
Title |
File |
| Vol 5, No 2-2 (2006): Special Issue |
TECHNICAL SCIENCES |
Automated system of gas turbine engines termogazdynamic calculation and analysis |
(Rus)
|
| Vol 5, No 2-2 (2006): Special Issue |
TECHNICAL SCIENCES |
The method of bypass engines turbocompressors structural-geometric parameters matching |
(Rus)
|
| Vol 5, No 2-2 (2006): Special Issue |
TECHNICAL SCIENCES |
Automated variant aircraft GTE turbocompressor flow path designing |
(Rus)
|
| Vol 5, No 2-2 (2006): Special Issue |
TECHNICAL SCIENCES |
Method of gas turbine engine control program and law optimization with accordance to efficiency parameters of aircraft |
(Rus)
|
| Vol 5, No 2-2 (2006): Special Issue |
TECHNICAL SCIENCES |
Perfection of operational characteristics calculation techniques for the decision of task of gas turbine engine control program optimization |
(Rus)
|
| Vol 11, No 5-1 (2012): Special Issue |
CONFERENCE MATERIALS |
Investigation of relative geometric parameters influence on bypass engine mass |
(Rus)
|
| Vol 11, No 5-1 (2012): Special Issue |
CONFERENCE MATERIALS |
Methods and means of aircraft gas turbine engine conceptual design underlying the CAE system «ASTRA» |
(Rus)
|
| Vol 11, No 5-1 (2012): Special Issue |
CONFERENCE MATERIALS |
Problem formulation of bypass engine parameters optimization with a preselected gas generator |
(Rus)
|
| Vol 11, No 5-1 (2012): Special Issue |
CONFERENCE MATERIALS |
Influence of the initial design data uncertainty on the choice of optimal working process parameters of gas turbine engine |
(Rus)
|
| Vol 11, No 5-1 (2012): Special Issue |
CONFERENCE MATERIALS |
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria |
(Rus)
|
| Vol 11, No 3-2 (2012): Special Issue |
CONFERENCE MATERIALS |
The task of creating the bypass engines of various thrust levels using the given gas generator |
(Rus)
|
| Vol 11, No 3-3 (2012): Special Issue |
CONFERENCE MATERIALS |
Fulfilment of initial design level of gas turbine engine using the methods of «ASTRA» CAE system |
(Rus)
|
| Vol 15, No 4 (2016) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Peculiarities of computer modeling of the working process in small gas turbine engines |
(Rus)
|
| Vol 10, No 3-3 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Dataware of virtual lab for gas turbine engine testing |
(Rus)
|
| Vol 10, No 3-3 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Concept of construction of virtual lab for gas turbine engine testing |
(Rus)
|
| Vol 10, No 3-4 (2011): Special Issue |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Preliminary study of principles of effective efficiency change of turboshaft engines of various schemes with heat recovery and intermediate cooling of working medium |
(Rus)
|
| Vol 18, No 3 (2019) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines |
(Rus)
|
| Vol 19, No 3 (2020) |
MECHANICAL ENGINEERING |
Improving the efficiency of aviation turbofan engines by using an intercooler and a recuperative heat exchanger |
(Rus)
|
| Vol 19, No 4 (2020) |
AIRCRAFT AND SPACE ROCKET ENGINEERING |
The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters |
(Rus)
|
| Vol 20, No 3 (2021) |
JUBILEES OF SCIENTISTS |
Artificial intelligence in aircraft design and the role of professor V.G. Maslov’s scientific school in the process of its development |
(Rus)
|
