STUDY OF UNSTABLE COMBUSTION IN THE COMBUSTION CAMERA OF THE ROCKET ENGINE
The phenomenon of instability of the combustion process, which has received the name “vibration burning” in the Russian literature, is one of the difficult problems that engine building has faced when creating the first liquid propellant rocket engines. As a rule, vibrational combustion leads to the destruction of the rocket engine, which was the reason for the intensive study of the instability of combustion and the development of ways to eliminate it.