Experimental Realization of H₂/Air Continuous Rotating Detonation in a Cylindrical Combustor

Abstract

Results of experimental studies on a H₂/air continuous rotating detonation engine (CRDE) in an annular combustor are presented. A tangentially injected H₂/O₂ hotshot jet is used to ignite the engine. H₂/air continuous rotating detonations are realized at a wide range of total mass flow and equivalence ratio conditions. The detonation propagation modes of all the tests can be divided into four kinds: two-wave, hybrid two/one wave, one-wave, and transient one wave. The mean propagation velocities of the two-wave and one-wave modes are in the range 1365–1476 m/s and 1606–1791 m/s, respectively. The propagation mode and velocity are influenced by both the total mass flow rate and equivalence ratio. Detonation wave propagation processes of the two-wave and one-wave modes are also observed, which further demonstrates the realization of CRDE.

Keywords:

• Continuous rotating detonation
• H₂/air mixture
• Propagation mode
• Propagation velocity

ACKNOWLEDGMENTS

This work is supported by the National Nature Science Foundation of the People's Republic of China through Grant Nos. 90816016 and 91016028.

Notes

× = corresponding parameter does not exist.

× = corresponding parameter does not exist.