Research on H2/Air rotating detonation in the hollow chamber with double injection.

In order to investigate the relationship between high frequency tangential instability and continuous rotating detonation, series of H 2 /Air rotating detonations are experimentally achieved in the hollow chamber with double injection sections. In the center part, gaseous H 2 and air injected by co-axial injector. Near the outer wall, the same propellants are injected in the form of slit-orifice collision. By keeping the total air mass flow rate approximately constant, varying the mixture of the inner and outer injection, series experiments are conducted in the test model with or without Laval nozzle. The results verify the possibility of rotating detonation in the hollow chamber with co-axial injector. To clarify the relationship between continuous rotating detonation and high frequency tangential combustion instability, the intrinsic frequencies of the test model are captured to be compared with propagation frequencies of detonation waves. The results show that they are close to each other when enough propellant assembled near the outer wall. In the combustor, the flame direction in constant pressure mode can change itself into rotating direction spontaneously. The results indicate that rotating detonation is an implication to high frequency tangential instability. • The results verify the possibility of rotating detonation in the hollow chamber with co-axial injector. • The key factor to forming detonation wave with co-axial injector has been discussed. • The results indicate that rotating detonation is an implication to high frequency tangential instability. [ABSTRACT FROM AUTHOR]