Bowen Wang

Experimental investigation of a shock divider for enhancing turbine performance under pulse detonation gas impact

Abstract To mitigate turbine performance degradation caused by the highly pulsating exhaust from a pulse detonation combustor (PDC) in pulse detonation turbine engines, a shock divider was employed in this study to regulate the detonation gas. An asymmetric dual-channel shock divider was designed and manufactured, and...