| 双模态超燃冲压发动机研究进展 |
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| 引用本文： | 乐嘉陵,胡欲立,刘陵.双模态超燃冲压发动机研究进展[J].实验流体力学,2000,14(1):1-12. |
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| 作者姓名： | 乐嘉陵 胡欲立 刘陵 |
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| 作者单位： | 1. 中国空气动力研究与发展中心,四川,绵阳,621000
2. 西北工业大学,陕西,西安,710072 |
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| 摘 要： | 通过对各种发动机性能的对比分析 ,认为双模态超燃冲压发动机非常适合作为高超声速飞行器的动力推进装置。国内外的实验研究和数值模拟的结果揭示了如何实现双模态超燃冲压的模态转换
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| 关 键 词： | 高超声速飞行器 双模态超燃冲压发动机 实验 数值模拟 |
| 修稿时间： | 1999-12-15 |
Investigation of possibilities in developing dual-mode scramjets |
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| LE Jia-ling,HU Yu-li,LIU Ling.Investigation of possibilities in developing dual-mode scramjets[J].Experiments and Measur in Fluid Mechanics,2000,14(1):1-12. |
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| Authors: | LE Jia-ling HU Yu-li LIU Ling |
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| Abstract: | Dual mode scramjet are considered as engines suitable for hypersonic vehicles by the comparison and analysis of performances of kinds of engines. The results of experimental research and numerical simulation at home and abroad reveal how to realize the mode transition. On the basis of relying on domestic existing condition and drawing lessons from overseas results, dual mode scramjets will be developed and tested at home in the future. |
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| Keywords: | hypersonic vehicle dual mode scramjet experiment numerical simulation |
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