机译:入口温度驱动的超临界燃烧型液化液化燃烧器中的燃烧型燃烧装置
Beihang Univ Coinnovat Ctr Adv Aeroengine Natl Key Lab Sci &
Technol Aeroengine Aerothermod Sch Energy &
Power Engn Beijing 100083 Peoples R China;
Imperial Coll London Dept Mech Engn London SW7 2AZ England;
Imperial Coll London Dept Mech Engn London SW7 2AZ England;
Beihang Univ Coinnovat Ctr Adv Aeroengine Natl Key Lab Sci &
Technol Aeroengine Aerothermod Sch Energy &
Power Engn Beijing 100083 Peoples R China;
Beihang Univ Coinnovat Ctr Adv Aeroengine Natl Key Lab Sci &
Technol Aeroengine Aerothermod Sch Energy &
Power Engn Beijing 100083 Peoples R China;
Beihang Univ Coinnovat Ctr Adv Aeroengine Natl Key Lab Sci &
Technol Aeroengine Aerothermod Sch Energy &
Power Engn Beijing 100083 Peoples R China;
Univ Connecticut Dept Mech Engn Storrs CT 06269 USA;
LPP combustor; Spray flame; Supercrtical bifurcation; Inlet temperature; Combustion instabilities;
机译:入口温度驱动的超临界燃烧型液化液化燃烧器中的燃烧型燃烧装置
机译:稀薄预混旋流燃烧室进气道几何形状对燃烧不稳定性影响的数值研究
机译:稀薄预混预蒸发燃烧器的燃烧振荡特性和火焰结构
机译:稀薄预混预蒸发(LPP)燃烧器的当量比波动测量及其与燃烧不稳定性的关系
机译:燃烧不稳定性:贫油预混燃烧器中氢气影响的实验研究。
机译:声激励对燃烧不稳定性的影响氢甲烷稀混合旋流火焰
机译:开源代码硅料燃烧燃气燃烧器燃烧不稳定性的案例研究
机译:分析稀薄预混/预蒸发燃烧器中的燃料汽化,燃料/空气混合和燃烧