The necessity about using supersonic combustion ramjet ( scramjet ) for the single stage to orb (?) t aerospace plane is demonstrated. 本文首先说明了单级入轨的空天飞机采用超声速燃烧冲压发动机的必要性。
The internal flow fields of supersonic combustion ramjet ( scramjet ) combustion chamber with strut or normal wall injectors are simulated numerically by using the Favre-averaged Navier-Stokes equations with the Baldwin-Lomax algebraic turbulence model. 应用含组分守恒方程的质量平均Navierstokes方程和BL代数湍流模型,数值模拟了后台阶构型燃烧室在采用台阶上游支板引射和壁面垂直引射燃料时的内部流场。
Numerical Simulation on Supersonic Combustion of Fuel-rich Gas for a Dual Combustor Ramjet Simulation and Experiment of Two-Phase Mixing and Combustion in the Scramjet Combustor 双燃烧室冲压发动机富油燃气超声速燃烧数值模拟超燃冲压发动机燃烧室两相流混合燃烧过程仿真及实验研究
Analysis of the hydrogen combustion field in scramjet dual-cavity combustor Numerical Simulation on Supersonic Combustion of Fuel-rich Gas for a Dual Combustor Ramjet 超燃冲压发动机双凹腔燃烧室氢气燃烧流场分析双燃烧室冲压发动机富油燃气超声速燃烧数值模拟
Investigation on supersonic combustion of fuel-rich hot gas as reacting jets in ramjet / scramjet combustor 双燃式冲压发动机中富油燃气射流的超燃研究