| 进水方式对水冲压发动机性能的影响 |
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| 引用本文： | 霍东兴,何国强,陈林泉,王建儒,陆贺建.进水方式对水冲压发动机性能的影响[J].固体火箭技术,2010,33(1). |
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| 作者姓名： | 霍东兴 何国强 陈林泉 王建儒 陆贺建 |
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| 作者单位： | 1. 西北工业大学航天学院,西安,710072
2. 中国航天科技集团公司第四研究院第四十一所固体火箭发动机燃烧、热结构与内流场国防科技重点实验室,西安,710025 |
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| 基金项目： | 自然科学基金项目(50676087) |
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| 摘 要： | 在一次燃气参数及总水燃比相同的情况下,研究了进水方式对水冲压发动机性能的影响,所得结论得到了试验结果的部分验证。研究表明,要使发动机获得较高比冲,进水方式的设计至少应该遵循两个原则——一次进水流量和活性铝粉流量接近1∶1;后部进水位置尽量靠前,以使所有水雾都能完全蒸发。
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| 关 键 词： | 水冲压发动机 进水方式 雾化喷嘴 铝水反应 |
Effects of water spray mode on water ramjet performance |
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| HUO Dong-xing,HE Guo-qiang,CHEN Lin-quan,WANG Jian-ru,LU He-jian.Effects of water spray mode on water ramjet performance[J].Journal of Solid Rocket Technology,2010,33(1). |
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| Authors: | HUO Dong-xing HE Guo-qiang CHEN Lin-quan WANG Jian-ru LU He-jian |
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| Institution: | 1.Coll.of Astronautics;Northwestern Polytechnical Univ.;Xi'an 710072;China;2.The National Key Laboratory of Combustion;Thermostructure and Flow of SRM;The 41st Institute of the Fourth Academy of CASC;Xi'an 710025;China |
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| Abstract: | The effects of water spray mode on water ramjet performance were studied under the same fuel gas parameters and to-tal water fuel ratios conditions. The conclusions were validated partially by the test data, The results show that at least two principles should be obeyed during designing the water spray mode for obtaining higher specific impulse, namely,mass flow ratios of H_2O and Abstract should be nearly 1: 1 ,and rear water spray location should be possibly close to head so as to make water fog evaporated com-pletely. |
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| Keywords: | water ramjet water spray mode atomizing nozzle aluminum-water reaction |
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