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水冲压发动机热力计算
引用本文:田维平,蔡体敏,陆贺建,高波.水冲压发动机热力计算[J].固体火箭技术,2006,29(2):95-98.
作者姓名:田维平  蔡体敏  陆贺建  高波
作者单位:1. 西北工业大学航天学院,西安,710072;中国航天科技集团公司四院,西安,710025
2. 西北工业大学航天学院,西安,710072
3. 中国航天科技集团公司四院,西安,710025
摘    要:简述了水冲压发动机化学平衡与非化学平衡热力计算方法及相应的适用条件,计算了试验发动机补燃室温度,并与试验数据进行了对比分析。分析结果表明,该热力计算方法适用于水冲压发动机。用热力计算方法可确定水冲压发动机最佳水燃比,进而指导水冲压发动机的设计和试验。

关 键 词:水冲压发动机  热力计算  化学平衡计算  非化学平衡计算
文章编号:1006-2793(2006)02-0095-04
收稿时间:2005-12-05
修稿时间:2006-01-11

Thermodynamic calculation for water ramjet
TIAN Wei-ping,CAI Ti-min,LU He-jian,GAO Bo.Thermodynamic calculation for water ramjet[J].Journal of Solid Rocket Technology,2006,29(2):95-98.
Authors:TIAN Wei-ping  CAI Ti-min  LU He-jian  GAO Bo
Abstract:Thermodynamic calculation method of chemical equilibrium and chemical non-equilibrium for water ramjet together with corresponding applicable conditions were introduced.Then the temperature in the ramjet combustor was calculated and compared with experimental data.The analysis results show that the calculation method is appliable for water ramjet.Thermodynamic calculation method can be used to determine the optimum water-fuel ratio of water ramjet so as to provide reference to design and test of water ramjet.
Keywords:water ramjet  thermodynamic calculation  chemical equilibrium calculation  chemical non-equilibrium calculation
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