Effects of Strake Configuration on Ram-Rotor Performance

Journal of Propulsion Technology ›› 2017, Vol. 38 ›› Issue (3): 710-720.

• Electric Propulsion and Other Advanced Propulsion • Previous Articles

Effects of Strake Configuration on Ram-Rotor Performance

Marine Engineering College，Dalian Maritime University，Dalian 116026，China,Marine Engineering College，Dalian Maritime University，Dalian 116026，China,Marine Engineering College，Dalian Maritime University，Dalian 116026，China and Marine Engineering College，Dalian Maritime University，Dalian 116026，China

Published:2021-08-15

隔板型式对旋转冲压压缩转子性能的影响

韩吉昂,孙云,钟兢军,管健

大连海事大学轮机工程学院，辽宁大连 116026,大连海事大学轮机工程学院，辽宁大连 116026,大连海事大学轮机工程学院，辽宁大连 116026,大连海事大学轮机工程学院，辽宁大连 116026

作者简介:韩吉昂，男，博士，副教授，研究领域为发动机气动力学。
基金资助:
国家自然科学基金(51406022)；辽宁省自然科学基金(2013020129)；辽宁省教育厅科学研究一般项目

Abstract

Abstract: In order to improve the overall performance of the ram-rotor，different strake schemes were obtained by changing the configuration of the ram-rotor’s fore segment and back segment. Then FLUENT software was adopted to simulate the flow field of different strake schemes. The results show that changing the strake fore segment’s configuration can change the shock wave structure of the ram-rotor’s leading edge and the inlet mass flow，and then affect the overall performance of the ram-rotor. Changing the strake back segment’s configuration can change the flow field structure of the ram-rotor and affect its compression capacity. Scheme combing optimal strake fore and back segment has the best performance whose total pressure ratio and efficiency increased by 12.0%，7.1% compared with the original scheme respectively.

Key words: Strake configuration；Ram-rotor；Performance；Flow structure；Numerical research

摘要： 为了改善旋转冲压压缩转子的总体性能，通过改变隔板前、后段的型式获得不同的隔板改型方案，并利用FLUENT流体计算软件对采用不同隔板改型方案的旋转冲压压缩转子进行了数值研究。结果表明，改变隔板前段型式可以改变隔板前缘激波和进气流量，进而影响旋转冲压压缩转子的总体性能；改变隔板后段型式，可以改变旋转冲压压缩转子的流场结构，并影响其增压能力；融合隔板前、后段最佳型式的隔板组合改型方案对旋转冲压压缩转子性能的提升最大，其总压比和效率相较于原型分别提升了12.0%和7.1%。

关键词: 隔板型式；旋转冲压压缩转子；性能；流场结构；数值研究

HAN Ji-ang,SUN Yun,ZHONG Jing-jun,GUAN Jian. Effects of Strake Configuration on Ram-Rotor Performance[J]. Journal of Propulsion Technology, 2017, 38(3): 710-720.

韩吉昂,孙云,钟兢军,管健. 隔板型式对旋转冲压压缩转子性能的影响[J]. 推进技术, 2017, 38(3): 710-720.

References

[1] Lawlor S P, Hinkey J B, Mackin S G, et al. Supersonic Compression Stage Design&Test Results[R]. IMECE 2004-59914.
[2] Grosvenor A D, Taylor D A, Bucher J R, et al. Measured and Predicted Performance of a High Pressure Ratio Supersonic Compressor Rotor[R]. ASME 2008-GT-50150.
[3] Grosvennor A D, Brown P M, Lawlor S P. Desigh Methodology and Predicted Performance for a Supersonic Compressor Stage[R]. ASME 2006-GT-90409.
[4] Steele R P, Baldwin P, Kesseli J. Insertion of Shock Wave Compression Technology into Micro Turbine for Increased Efficiency and Reduced Costs[R]. ASME 2005-GT-68203.
[5] Lawlor S P, Baldwin P. Conception Design of a Supersonic CO₂ Compressor[R]. ASME 2005-GT-68349.
[6] 王云. 新概念旋转冲压发动机基础性探索研究[D]. 南京:南京航空航天大学, 2005.
[7] 肖翔, 赵晓路, 徐建中. 高压比旋转冲压叶轮研究[J]. 工程热物理学报, 2008, 29(5): 759-762.
[8] 肖翔, 刘锡阳, 赵晓路, 等. ?对转冲压压气机冲压叶栅实验研究[J]. ?工程热物理学报, 2009, 30(11):1837-1840.
[9] 扈延林, 唐菲, 赵庆军, 等. 冲压叶栅边界层抽吸处理分析[J]. 推进技术, 2012, 33(3): 356-362. (HU Yan-lin, TANG Fei, ZHAO Qing-jun, et al. Numerical Investigation on the Effects of Boundary Layer Suction in a Ramrotor Cascade[J]. Journal of Propulsion Technology, 2012, 33(3): 356-362.)
[10] 扈延林, 孙小磊, 唐菲, 等. 冲压转子流场和轮毂抽吸处理分析[J]. 工程热物理学报, 2011, 32(7): 1111-1114.
[11] 孙小磊, 扈延林, 徐建中. 叶顶间隙对冲压叶轮激波结构的影响[J]. 工程热物理学报, 2012, 33(1): 35-38.
[12] 韩吉昂, 严红明, 钟兢军, 等. 旋转冲压压缩转子二维进气流道数值研究[J]. 航空动力学报, 2008, 23(6): 1054-1060.
[13] 韩吉昂, 钟兢军, 严红明. 旋转冲压压缩转子三维进气流道数值研究[J]. 航空动力学报, 2009, 24(5): 1079-1088.
[14] 王国栋. 旋转冲压压缩转子激波系配置研究[D]. 大连:大连海事大学, 2012.
[15] 杨凌. 旋转冲压压缩转子结构与性能研究[D]. 大连:大连海事大学, 2011.
[16] 韦狄. 附面层抽吸位置对旋转冲压压缩转子影响研究[D]. 大连:大连海事大学, 2013.
[17] 钟兢军, 韩吉昂, 杨凌. 旋转冲压压缩转子研究进展及发展前景[J]. 航空动力学报, 2011, 26(10): 2293-2301.
[18] 韩吉昂, 管健, 钟兢军, 等. 旋转冲压压缩转子试验系统通流部分数值研究[J]. 推进技术, 2016, 37(4): 758-768. (HAN Ji-ang, GUAN Jian, ZHONG Jing-jun, et al. Numerical Research on Flow Passage of Ram-Rotor Test System[J]. Journal of Propulsion Technology, 2016, 37(4): 758-768.)
[19] 韩吉昂, 管健, 钟兢军, 等. 旋转冲压压缩转子试验系统变工况数值研究[J]. 航空动力学报, 2015, 30(10): 2425-2439.
[20] Prince D C. Three-Dimensional Shock Structures for Transonic/Supersonic Compressor Rotors[J]. Journal of Aircraft, 1980, 17(1): 28-37.
[21] Benini E, Biollo R. On the Aerodynamics of Swept and Leaned Transonic Compressor Rotors[R]. ASME 2006-GT-90547.
[22] 茅晓晨, 刘波, 张国臣, 等. 复合弯掠优化对跨声速压气机性能影响的研究[J]. 推进技术, 2015, 36(7): 996-1004. (MAO Xiao-chen, LIU Bo, ZHANG Guo-chen, et al. Effectiveness of Composite Optimization of Lean and Sweep on Transonic Compressor Performance[J]. Journal of Propulsion Technology, 2015, 36(7): 996-1004.)　　收稿日期:2016-05-05；修订日期:2016-06-23。基金项目:国家自然科学基金(51406022)；辽宁省自然科学基金(2013020129)；辽宁省教育厅科学研究一般项目 (L2013199)；辽宁省高校创新团队支持计划资助(LT2015004)。作者简介:韩吉昂,男,博士,副教授,研究领域为发动机气动力学。E-mail: hja6065@126.com(编辑:朱立影)

Effects of Strake Configuration on Ram-Rotor Performance

隔板型式对旋转冲压压缩转子性能的影响

PDF

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 0

Recommended Articles

Metrics

Comments