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Large eddy simulation of supersonic flow in ducts with complex cross-sections
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作者 Huifeng Chen Mingbo Sun +3 位作者 dapeng xiong Yixin Yang Taiyu Wang Hongbo Wang 《Theoretical & Applied Mechanics Letters》 CAS CSCD 2023年第6期432-440,共9页
Large Eddy Simulation(LES)has been employed for the investigation of supersonic flow characteristics in five ducts with varying cross-sectional geometries.The numerical results reveal that flow channel configurations ... Large Eddy Simulation(LES)has been employed for the investigation of supersonic flow characteristics in five ducts with varying cross-sectional geometries.The numerical results reveal that flow channel configurations exert a considerable influence on the mainstream flow and the near-wall flow behavior.In contrast to straight ducts,square-to-circular and rectangular-to-circular ducts exhibit thicker boundary layers and a greater presence of vortex structures.Given the same inlet area,rectangular-to-circular ducts lead to higher flow drag force and total pressure loss than square-to-circular ducts.Characterized by the substantial flow separation and shock waves,the"S-shaped duct shows significant vertically-asymmetric characteristics. 展开更多
关键词 SCRAMJET LES Complex cross-section Boundary layer
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Analysis of Capability Requirement of Dynamic Positioning System for Cargo Transfer Vessel at Sea 被引量:2
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作者 Kaiye Hu Yong Ding +2 位作者 Hongwei Wang dapeng xiong Di Yang 《Journal of Marine Science and Application》 CSCD 2019年第2期205-212,共8页
In response to the development of deep-sea oil and gas resources,which require a high degree of cooperation by crude oil transportation equipment,a new type of ship known as the cargo transfer vessel(CTV)has been deve... In response to the development of deep-sea oil and gas resources,which require a high degree of cooperation by crude oil transportation equipment,a new type of ship known as the cargo transfer vessel(CTV)has been developed.To provide a theoretical reference for the design and equipment of the CTV’s dynamic positioning system,in this paper,we take the new deepwater CTVas the study object and theoretically and numerically analyze its operation,wind load,current load,wave load,and navigational resistance in a range of Brazilian sea conditions with respect to its positioning and towing modes.We confirm that our proposed method can successfully calculate the total environmental load of the CTVand that the CTV is able to operate normally under the designed sea conditions. 展开更多
关键词 CARGO TRANSFER VESSEL Wind LOAD Current LOAD Wave LOAD DP CAPABILITY Oil TRANSFER operation
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马赫数6飞行条件圆截面超燃冲压发动机流动燃烧特征分析
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作者 于江飞 汤涛 +4 位作者 闫博 汪洪波 杨揖心 熊大鹏 孙明波 《航空学报》 EI CAS CSCD 北大核心 2024年第14期215-228,共14页
本文基于RANS方法对马赫数6飞行条件下的乙烯燃料圆截面超燃冲压发动机燃烧流场开展了数值研究,计算中采用了压力相关的火焰面/进度变量模型,得到的数值结果与试验吻合,并据此分析了0.18和0.06当量比工况的火焰结构和燃烧特征。计算表明... 本文基于RANS方法对马赫数6飞行条件下的乙烯燃料圆截面超燃冲压发动机燃烧流场开展了数值研究,计算中采用了压力相关的火焰面/进度变量模型,得到的数值结果与试验吻合,并据此分析了0.18和0.06当量比工况的火焰结构和燃烧特征。计算表明,0.18当量比工况释热强度高,在流场中形成了热壅塞,并且预混燃烧和扩散燃烧共同主导了整体的释热。而0.06当量比工况流道中心仍是超声速状态,扩散火焰主导了整体的释热。2个工况中,射流背风区和轴对称凹腔都是重要的反应区,其中射流背风区释热强度高,而凹腔起到了增强混合和提高燃烧效率的重要作用。 展开更多
关键词 圆截面超燃冲压发动机 火焰面/进度变量模型 超声速燃烧 轴对称凹腔
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Effect of kerosene injection states on mixing and combustion characteristics in a cavity-based supersonic combustor 被引量:1
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作者 Xu LIU Peibo LI +6 位作者 Fei LI Hongbo WANG Mingbo SUN Chao WANG Yixin YANG dapeng xiong Yanan WANG 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2024年第4期308-320,共13页
It has been found that the static pressure distribution along the axial direction of liquid kerosene is lower than that of the gaseous kerosene under the same flow condition and overall equivalent ratio from previous ... It has been found that the static pressure distribution along the axial direction of liquid kerosene is lower than that of the gaseous kerosene under the same flow condition and overall equivalent ratio from previous studies.To further investigate this phenomenon,a compressible two-phase parallel simulation method is utilized to analyze the mixing and combustion characteristics of gaseous and liquid kerosene jets in a cavity-based supersonic combustor.The numerical results are consistent with the experiments and demonstrate that gaseous injection leads to a cavity shear layer that dives deeper into the cavity,forming two recirculation zones in the front and rear of the cavity.In contrast,the cavity shear layer is closer to the mainstream during liquid injection,and only a large recirculation zone is formed in the rear of the cavity.As a result of the cavity shear layer and the recirculating flow,the fuel vapor of gaseous injection accumulates in the front of the cavity,while for the liquid injection,the fuel vapor disperses in the cavity,cavity shear layer,and the region above,and the rear of the cavity has a higher fuel vapor concentration than the front.This unique fuel distribution causes the combustion area to be concentrated in the cavity during the gaseous injection but dispersed inside and downstream of the cavity during the liquid injection.As a result,forming a thermal throat under the same conditions is more challenging during liquid injection,and the generated static pressure distribution is lower than that during the gaseous injection. 展开更多
关键词 Gaseous injection Liquid injection Mixing process Combustion Supersonic flow
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