Combustion in Supersonic Flow in a Two-Section Channel with Side Supply of Compressed Air and Hydrogen
摘要
The control of combustion by throttling jets in a two-section channel with high-speed flow was studied numerically. Pulses of the first throttling jet were used to produce intense transonic combustion of hydrocarbon fuel in the first section. Side fuel supply was used to maintain the combustion regime before the channel expansion after the switching-off of the first jet. The fuel combustion efficiency in the second section was increased using a second throttling jet. The Reynolds-averaged Navier–Stokes equations closed by the