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On the effects of fuel inlet configurations and equivalence ratio to the pre-heating stage of a liquid fuelled flameless swirl combustor

机译：燃料入口配置与等效比对液体燃料无焰旋流燃烧器预热阶段的影响

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Adam Kasani; Mazlan Abdul Wahid; Muhammad Amri Mazlan; Aminuddin Saat; Mohd Yasin;
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1. Effects of Inlet Air Swirl and Spray Cone Angle on Combustion and Emission Performance of a Liquid Fuel Spray in a Gas Turbine Combustor [J] . D Chatterjee, A Datta, A K Ghosh, Journal of the Institution of Engineers (Inida). Aerospace Engineering Division Board . 2004,第Nov期

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2. Experimental Investigation on the Effects of Swirlers Configurations and Air Inlet Partitioning in a Partially Premixed Double High Swirl Gas Turbine Model Combustor [J] . Amir Mardani, Benyamin Asadi Rekabdarkolaei, Hamed Rezapour Rastaaghi Journal of Energy Resources Technology . 2021,第1期

机译：旋流器配置与空气入口分配在部分预混的双旋风燃气涡轮机模型燃烧器中的实验研究
3. Experimental study of equivalence ratio and fuel flow rate effects on nonlinear thermoacoustic instability in a swirl combustor [J] . Zhao He, Li Guoneng, Zhao Dan, Applied Energy . 2017,第deca15期

机译：当量比和燃料流量对旋流燃烧室非线性热声不稳定性影响的实验研究
4. Tests of a Fixed-Geometry Inlet-Combustor Configuration for a Hydrocarbon-Fueled, Dual-Mode Scramjet [C] . Earl H. Andrews, Carl A. Trexler, Saied Emami 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference June 27-29, 1994/Indianapolis, IN . -1

机译：碳氢燃料双模超燃冲压发动机固定几何形状的进气燃烧室配置的测试
5. Turbulent Non-premixed Swirl-Stabilized Flames of Gaseous and Liquid Fuels in a Gas Turbine Model Combustor [D] . Chatterjee, Sandipan 2019

机译：燃气轮机模型燃烧器中气态和液态燃料的湍流非预混涡流稳定火焰
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7. Experimental study of equivalence ratio and fuel flow rate effects on nonlinear thermoacoustic instability in a swirl combustor [O] . He Zhao, Guoneng Li, Dan Zhao, 2017

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8. EFFECT OF PRIMARY-ZONE EQUIVALENCE RATIO AND HYDROGEN ADDITION ON EXHAUST EMISSION IN A HYDROCARBON-FUELED COMBUSTOR [R] . Carl T. Norgren, Robert D. Ingebo 1974

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On the effects of fuel inlet configurations and equivalence ratio to the pre-heating stage of a liquid fuelled flameless swirl combustor

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