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二元亚燃冲压发动机高空模拟扩压器气动设计
引用本文:庄欢,刘志友,马前容,田金虎.二元亚燃冲压发动机高空模拟扩压器气动设计[J].燃气涡轮试验与研究,2011(3):50-53.
作者姓名:庄欢  刘志友  马前容  田金虎
作者单位:中国燃气涡轮研究院,四川江油,621703
摘    要:根据某型二元亚燃冲压发动机连管试验对高空舱内环境压力的要求,考虑高空台现有的抽气能力,充分利用冲压发动机排出燃气的能量,以提高模拟高度、节约能源、扩大高空台工作范围为目的,使用商业数值计算软件设计了一种高空模拟扩压器,并确定了最优的扩压器结构形式、结构参数和引射间距。

关 键 词:扩压器  冲压发动机  高空模拟  数值计算

Aerodynamic Design on High Altitude Simulation Diffuser of Two-Dimensional Ramjet Engine
ZHUANG Huan,LIU Zhi-you,MA Qian-rong,TIAN Jin-hu.Aerodynamic Design on High Altitude Simulation Diffuser of Two-Dimensional Ramjet Engine[J].Gas Turbine Experiment and Research,2011(3):50-53.
Authors:ZHUANG Huan  LIU Zhi-you  MA Qian-rong  TIAN Jin-hu
Institution:(China Gas Turbine Establishment,Jiangyou 621703,China)
Abstract:In this paper, an exhaust Omuser was designed by numerical calculation software according to the requirement of the two-dimensional ramjet experiments. The new diffuser could make the best of the gas energy, send up the simulative altitude, economize ene
Keywords:diffuser  ramjet engine  high altitude simulation  numerical calculation
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