首页|The Design and Performance of a High Temperature Rise Combustor for Wind Tunnel
The Design and Performance of a High Temperature Rise Combustor for Wind Tunnel
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国家科技期刊平台
NETL
NSTL
万方数据
维普
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.
high temperature riseevaporatorwind tunnelcombustoraviation kerosene
Zhang Rongchun、Fan Weijun
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National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
国家科技期刊平台
NSTL
万方数据
维普
