| 引用本文: | 赵一龙,赵玉新,王振国,易仕和.超声速型面可控喷管设计方法[J].国防科技大学学报,2012,34(5):1-4.[点击复制] |
| ZHAO Yilong,ZHAO Yuxin,WANG Zhenguo,YI Shihe.Designing method of supersonic nozzle with controllable contour[J].Journal of National University of Defense Technology,2012,34(5):1-4[点击复制] |
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| 超声速型面可控喷管设计方法 |
| 赵一龙,赵玉新,王振国,易仕和 |
| (国防科技大学 航天与材料工程学院，湖南 长沙 410073) |
| 摘要: |
| 提出了基于B-Spline曲线和特征线方法的超声速型面可控喷管设计方法，通过设置喷管轴向马赫数分布可以灵活地调整喷管的型面形状。数值验证结果表明，该方法不仅可以设计出高品质的喷管出口流场，而且能够实现喷管型面的灵活调整，可以获得长度与最短长度喷管一致，但流场品质更优的喷管。 |
| 关键词: 超声速 喷管设计 B-Spline曲线 特征线方法 |
| DOI： |
| 投稿时间：2012-03-06 |
| 基金项目:国家自然科学基金资助项目（11072264） |
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| Designing method of supersonic nozzle with controllable contour |
| ZHAO Yilong,ZHAO Yuxin,WANG Zhenguo,YI Shihe |
| (College of Aerospace and Materials Engineering，National University of Defense Technology，Changsha 410073，China) |
| Abstract: |
| A designing method of supersonic nozzle with controllable contour based on B-Spline curve and characteristic line algorithm is proposed. The contour of the nozzle was adjusted by assigning the distribution of Mach number on the nozzle’s axis. The reliability of the designing method was validated by numerical simulation, which shows that the outflow of the nozzle with high quality can be produced and the contour can be adjusted freely. The result also shows that the nozzle designed by the proposed method can produce better flow than the minimal length nozzle(MLN) with the same length. |
| Key words: supersonic nozzle design B-Spline curve characteristic line algorithm |
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