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变几何超燃冲压发动机优化设计研究
引用本文:李建平,宋文艳,柏韧恒,李卫强. 变几何超燃冲压发动机优化设计研究[J]. 世界科技研究与发展, 2012, 34(1): 50-54
作者姓名:李建平  宋文艳  柏韧恒  李卫强
作者单位:1. 西北工业大学动力与能源学院,西安,710072
2. 西北工业大学理学院,西安,710072
基金项目:西北工业大学基础研究基金
摘    要:构建了包括前体/进气道、燃烧室、尾喷管/后体的全流道超燃冲压发动机性能计算程序和优化设计平台,对性能计算程序的适用性进行了验证.进行了氢燃料变几何燃烧室的全流道超燃冲压发动机优化设计.设计结果表明,变几何燃烧室超燃冲压发动机性能得到提高.

关 键 词:超燃冲压发动机  优化设计  变几何燃烧室  比冲

Researches on Optimization Design of Variable-geometry Scramjet
LI Jianping , SONG Wenyan , BO Renheng , LI Weiqiang. Researches on Optimization Design of Variable-geometry Scramjet[J]. World Sci-tech R & D, 2012, 34(1): 50-54
Authors:LI Jianping    SONG Wenyan    BO Renheng    LI Weiqiang
Affiliation:1. School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072 2. School of Science, Northwestern Polytechnical University, Xi'an 710072 )
Abstract:A performance calculation program and the optimization design platform of full-flowpath scramjet were set up,including the three main parts of forebody/inlet, eombustor and nozzle/afterbody. Aiming at hydrogen fueled, the full-flowpath scramjet configuration optimization design was performed based on the optimization design platform. The results indicated that the performance of variable-geometry combustor scramjet is improved.
Keywords:scramjet  optimization design  variable-geometry combustor  specific impulse
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