Автор туралы ақпарат
Yakovlev, N. N.
| Шығарылым | Бөлім | Атауы | Файл |
| Том 478, № 2 (2018) | Physical Chemistry | Rocket Engine with Continuous Detonation Combustion of the Natural Gas–Oxygen Propellant System | |
| Том 481, № 1 (2018) | Physical Chemistry | Wind Tunnel Testing of a Detonation Ramjet Model at Approach Air Stream Mach Number 5.7 and a Stagnation Temperature of 1500 K |