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The Design and Performance of a High Temperature Rise Combustor for Wind Tunnel 被引量:1
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作者 Zhang Rongchun Fan Weijun 《Journal of Thermal Science》 SCIE EI CAS CSCD 2011年第6期556-562,共7页
A high-temperature-rise combustor that can be used in high-temperature wind tunnel is introduced in this study.Aviation kerosene is used in this type of combustor,with division combustion scheme and evaporator fuel-su... A high-temperature-rise combustor that can be used in high-temperature wind tunnel is introduced in this study.Aviation kerosene is used in this type of combustor,with division combustion scheme and evaporator fuel-supply device adopted.In the performance test under atmospheric pressure,when the inlet temperature is 500K and air flow is within the range of 1.5-3.0 kg/s,the outlet temperature can be precisely regulated within the range of 1050K-2100K.Moreover,higher uniformity of outlet temperature distribution and higher combustion efficiency can be achieved.After the long-time working in the wind tunnel,various components of the combustor,especially the combustor liners are checked without finding any anomaly such as thermal deformation. 展开更多
关键词 性能测试 燃烧室 温度上升 风洞 设计 出口温度 航空煤油 燃料供应
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