航天推进技术研究院主办
[1]李永洲,李哲,李光熙,等.ATR/冲压组合动力高超声速飞行器性能分析[J].火箭推进,2018,44(03):6-11.
LI Yongzhou,LI Zhe,LI Guangxi,et al.Performance analysis of hypersonic aircraft with ATR/ramjet combined power[J].Journal of Rocket Propulsion,2018,44(03):6-11.
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LI Yongzhou,LI Zhe,LI Guangxi,et al.Performance analysis of hypersonic aircraft with ATR/ramjet combined power[J].Journal of Rocket Propulsion,2018,44(03):6-11.
ATR/冲压组合动力高超声速飞行器性能分析
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
44
期数:
2018年03期
页码:
6-11
栏目:
研究与设计
出版日期:
2018-06-30
- Title:
- Performance analysis of hypersonic aircraft with ATR/ramjet combined power
- 文章编号:
- 1672-9374(2018)03-0006-06
- Keywords:
- hypersonic aircraft; combined cycle engine; ATR engine; ramjet; analysis of perfor-mance parameters
- 分类号:
- V231-34
- 文献标志码:
- A
- 摘要:
- 针对ATR/冲压并联组合动力的高超声速飞行器,按照典型弹道对其总体性能参数进行计算和分析。结果表明:ATR工作段飞行器的加速性能良好,尤其是在Ma2.0～3.5范围内。总航程随着推重比增加而迅速增加,而飞行时间差别很小,其中ATR工作阶段所占比例显著降低。总航程和飞行时间随着升阻比增加而显著增加,且影响最大的是冲压发动机工作的Ma6.0附近区域。上述研究从飞行器系统角度出发,进一步深化了对ATR发动机的认识。
- Abstract:
- For the hypersonic aircraft with ATR/ramjet parallel combined power, its overall performance parameters are calculated and analyzed according to a typical trajectory. The results show that the acceleration of the aircraft is good during the operating phase of ATR engine, especially in the range of Mach 2.0～3.5. The total flight range increases rapidly as the thrust-weight ratio increases, while the difference of flight time is very small, in which the proportion of ATR operating phase is significantly decreased. The total flight range and flight time increase significantly with the increase of lift-drag ratio, and a sharp increment turns up when Mach number reaches up to about 6.0. The above research further deepens the understanding of ATR engine from the view of aircraft system.
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备注/Memo
收稿日期:2017-11-12
基金项目:国家自然科学基金(11702205)
作者简介:李永洲(1984—),男,博士,研究领域为高超声速组合发动机设计和内流气体动力学
更新日期/Last Update:
2018-06-30