To investigate the problem of ethylene jet mixing and combustion in the scramjet at high Mach number(Ma = 8), numerical simulations were carried out for different equivalent ratios at cold and combustion conditions, i...To investigate the problem of ethylene jet mixing and combustion in the scramjet at high Mach number(Ma = 8), numerical simulations were carried out for different equivalent ratios at cold and combustion conditions, in which three-dimensional steady compressible RANS and k-ω SST turbulence model were adopted. It demonstrates that as the equivalence ratio increases from 0.42 to 1.08, the combustion becomes more intensified, and the higher backpressure pushes flame to propagate upstream. The supersonic combustion region in the combustor decreases from 92% to 85% with the increase of equivalence ratio from 0.42 to 1.08, resulting in the transition of the combustor from scram-mode to dual-mode. Both mixing and combustion efficiencies decrease by 35% and 16% respectively when the equivalence ratio increases from 0.42 to 1.08, indicating that the high equivalence ratio is unfavorable to the mixing and combustion processes. Combustion mode analysis reveals that the flame in the cavity under the high Mach number is dominated by non-premixed flames, i.e., more than 95% behaves as non-premixed mode, and the heat release is also mainly contributed by non-premixed flame. Increasing the equivalence ratio is beneficial to the thrust performance. Although the viscous force hardly changes with equivalence ratio, the percentage of pressure force used to balance the viscous force increases gradually,which limits the engine performance.展开更多
对大规模交直流网络下的高压直流控制保护系统进行参数优化设计,是保证灵活交流输电系统暂态性和稳定性良好的重要手段。目前由于实时仿真技术的网络节点受限、费用高等缺点,使其不适合此规模网络的试验和设计任务。文中基于ABB公司高...对大规模交直流网络下的高压直流控制保护系统进行参数优化设计,是保证灵活交流输电系统暂态性和稳定性良好的重要手段。目前由于实时仿真技术的网络节点受限、费用高等缺点,使其不适合此规模网络的试验和设计任务。文中基于ABB公司高压直流控制保护系统硬件结构特点和MACH2(modular advanced control for HVDC and SVC)系统运作机理,提出了等价实时离线仿真的实现原理和方法,使离线仿真达到实时仿真的效果;通过与实际工控机运行结果进行比对,验证了其有效性;同时对工程用高压直流控制中的电流控制功能进行了等价实时仿真。仿真结果分析表明,基于所提出的等价实时仿真原理和方法,利用商业通用的离线仿真软件,可高效地进行高压直流控制保护系统优化设计。展开更多
文摘To investigate the problem of ethylene jet mixing and combustion in the scramjet at high Mach number(Ma = 8), numerical simulations were carried out for different equivalent ratios at cold and combustion conditions, in which three-dimensional steady compressible RANS and k-ω SST turbulence model were adopted. It demonstrates that as the equivalence ratio increases from 0.42 to 1.08, the combustion becomes more intensified, and the higher backpressure pushes flame to propagate upstream. The supersonic combustion region in the combustor decreases from 92% to 85% with the increase of equivalence ratio from 0.42 to 1.08, resulting in the transition of the combustor from scram-mode to dual-mode. Both mixing and combustion efficiencies decrease by 35% and 16% respectively when the equivalence ratio increases from 0.42 to 1.08, indicating that the high equivalence ratio is unfavorable to the mixing and combustion processes. Combustion mode analysis reveals that the flame in the cavity under the high Mach number is dominated by non-premixed flames, i.e., more than 95% behaves as non-premixed mode, and the heat release is also mainly contributed by non-premixed flame. Increasing the equivalence ratio is beneficial to the thrust performance. Although the viscous force hardly changes with equivalence ratio, the percentage of pressure force used to balance the viscous force increases gradually,which limits the engine performance.
文摘对大规模交直流网络下的高压直流控制保护系统进行参数优化设计,是保证灵活交流输电系统暂态性和稳定性良好的重要手段。目前由于实时仿真技术的网络节点受限、费用高等缺点,使其不适合此规模网络的试验和设计任务。文中基于ABB公司高压直流控制保护系统硬件结构特点和MACH2(modular advanced control for HVDC and SVC)系统运作机理,提出了等价实时离线仿真的实现原理和方法,使离线仿真达到实时仿真的效果;通过与实际工控机运行结果进行比对,验证了其有效性;同时对工程用高压直流控制中的电流控制功能进行了等价实时仿真。仿真结果分析表明,基于所提出的等价实时仿真原理和方法,利用商业通用的离线仿真软件,可高效地进行高压直流控制保护系统优化设计。
