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面向飞机总体设计的开式转子发动机分析模型

张帅 余雄庆

张帅, 余雄庆. 面向飞机总体设计的开式转子发动机分析模型[J]. 航空动力学报, 2012, 27(8): 1801-1808.
引用本文: 张帅, 余雄庆. 面向飞机总体设计的开式转子发动机分析模型[J]. 航空动力学报, 2012, 27(8): 1801-1808.
ZHANG Shuai, YU Xiong-qing. Model of open rotor engine for aircraft conceptual design[J]. Journal of Aerospace Power, 2012, 27(8): 1801-1808.
Citation: ZHANG Shuai, YU Xiong-qing. Model of open rotor engine for aircraft conceptual design[J]. Journal of Aerospace Power, 2012, 27(8): 1801-1808.

面向飞机总体设计的开式转子发动机分析模型

基金项目: 南京航空航天大学科研基地创新创优基金(NJ2010006)

Model of open rotor engine for aircraft conceptual design

  • 摘要: 应用高速桨扇试验数据与涡轴核心机估算模型相结合的方法,建立了一种快速的、能用于飞机总体方案论证阶段的开式转子发动机分析模型.它使用少量的总体参数即可估算出开式转子发动机推力与耗油率特性、质量和外形尺寸,计算速度快.通过对比模型的估算结果与文献的试验数据,证明其精度能够满足飞机总体初步方案论证的要求,可用于评估采用开式转子发动机带来的收益.

     

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出版历程
  • 收稿日期:  2011-09-19
  • 刊出日期:  2012-08-28

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