Author Details
Зубанов, В. М., Самарский национальный исследовательский университет имени академика С.П. Королёва, Russian Federation
| Issue | Section | Title | File |
| Vol 15, No 4 (2016) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Method of transient simulation of combustion processes in a low-thrust rocket engine operating on gaseous hydrogen and oxygen |
 (Rus) |
| Vol 15, No 4 (2016) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Simulation of the work process of a two-stage pump with a first-stage hydraulic drive |
(Rus) |
| Vol 19, No 3 (2020) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Method of coordinating joint operation of air starter and auxiliary power unit and determining the gas turbine engine starting time |
(Rus) |
| Vol 22, No 1 (2023) | MECHANICAL ENGINEERING | Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade |
(Rus) |