Combustion performance of n-butane-fueled mesoscale annular combustor
The lower vapor pressure of n-butane than gaseous fuels, such as hydrogen, methane, and propane, enables its fuel containers to be compact and highly portable.
Yosuke SUENAGA, Hideki YANAOKA
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A deep learning-based approach for flow field prediction in a dual-mode combustor
Accurate acquisition of the distribution of flow parameters inside the supersonic combustor is of great significance for hypersonic flight control. It is an interesting attempt to introduce a data-driven model to a supersonic combustor for flow field ...
Chen Kong +4 more
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Unveiling soot volume fraction trends in model gas turbine RQL combustor at varying pressure using in-situ LII calibration technique [PDF]
Poorva Shrivastava +3 more
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Effects of a Three-Dimensional-Printed Atomizer Component on Fuel-Spray and Flame Characteristics of a Jet-Stabilized Compact Gas Turbine Combustor Fed With Liquid Fuels [PDF]
Haisol Kim, Jhon Pareja, Oliver Lammel
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Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor [PDF]
Xuejun Fan +4 more
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Combustion instability of pilot flame in a pilot bluff body stabilized combustor
Xiao Fu, Fujiang Yang, Zhihui Guo
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The Effect of Differentiating the Thermal Conductivity between Inner and Outer Walls on the Stability of a U-Bend Catalytic Heat-Recirculating Micro-Combustor: A CFD Study [PDF]
Valeria Di Sarli
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A micro-pulse detonation engine (μPDE) was designed and installed to a direct-connect scramjet combustor of Pusan National University (PNU-DCSC). The active excitation on the scramjet combustor was experimentally studied using the μPDE operating at ...
Keon-Hyeong Lee +3 more
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