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Journal of Projectiles, Rockets, Missiles and Guidance >
Study on Aerodynamic Prediction Method for Ventral Inlet Missile
Received date: 2017-08-11
Online published: 2025-05-30
The aerodynamic performance of the ventral inlet configuration missile is hard to predict due to the complex interferences between inlet and the outer flow field. To solve the problem in the conceptual design of the missile, based on DATCOM program and CFD numerical simulation, a method combining component built-up method and CFD-corrected results was developed. The results showed that the method was efficient, adaptive, and highly accurate; it has high application value in conceptual design of air-breathing missile.
Key words： air-breathing missile; aerodynamic prediction; ventral inlet
LI Xueping , CAO Yitao . Study on Aerodynamic Prediction Method for Ventral Inlet Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2018 , 38(3) : 129 -134 . DOI: 10.15892/j.cnki.djzdxb.2018.03.032
| [1] | 王起飞. 冲压发动机导弹进气道设计的几个问题[J]. 火箭推进,2004,30(2): 24-28. |
| [2] | 蔡飞超,陈凤明,徐东来,等. 宽Ma 数范围固定几何进气道设计问题研究[J]. 固体火箭技术,2010,33(2): 163-166. |
| [3] | KRIEGER R J,WILLIAMS J E,HOOD R F. A component buildup aerodynamic prediction approach for airbreathing missile[C]// AIAA. Proceedings of 21st Aerospace Sciences Meeting. Reston: AIAA, 1983: 1-19 |
| [4] | BLAKE W B. Missile datcom user’s manual: 1997 fortran 90 revision: AFRL-VA-WP-TR-1998-3009[R].[S. l.: s. n.], 1998. |
| [5] | VUKELICH S R,STOY S,BURNS K,et al. Missile dat-com final report: AFWAL-TR-86-3091.[R].[S. l.: s.n.], 1986. |
| [6] | 石清. 带进气道的面对称布局战术导弹气动特性工程估算[J]. 流体力学实验与测量,2004,18(2): 98-101. |
| [7] | 周岭,赵协和. 吸气式导弹气动力预计方法研究[J]. 空气动力学学报,2006,24(4): 491-494. |
| [8] | 何佳丽,梁国柱,邱伟. 飞行器气动计算方法的应用研究[J]. 航空计算技术,2008,38(1): 47-51. |
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