Author Details
Yakovlev, N. N.
| Issue | Section | Title | File |
| Vol 478, No 2 (2018) | Physical Chemistry | Rocket Engine with Continuous Detonation Combustion of the Natural Gas–Oxygen Propellant System | |
| Vol 481, No 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 |