Ignition and Flame Stabilization of a Strut-Jet RBCC Combustor with Small Rocket Exhaust
A Rocket Based Combined Cycle combustor model is tested at a ground direct connected rig to investigate the flame holding characteristics with a small rocket exhaust using liquid kerosene.The total temperature and the Mach number of the vitiated air flow, at exit of the nozzle are 1505 K and 2.6, respectively.The rocket base is embedded in a fuel i