Instantaneous and time-averaged flow structures around a blunt double-cone with or without supersonic film cooling visualized via nano-tracer planar laser scattering

doi:10.1088/1674-1056/22/1/014702

Chin. Phys. B ›› 2013, Vol. 22 ›› Issue (1): 14702-014702.doi: 10.1088/1674-1056/22/1/014702

• ELECTROMAGNETISM, OPTICS, ACOUSTICS, HEAT TRANSFER, CLASSICAL MECHANICS, AND FLUID DYNAMICS • 上一篇下一篇

Instantaneous and time-averaged flow structures around a blunt double-cone with or without supersonic film cooling visualized via nano-tracer planar laser scattering

朱杨柱, 易仕和, 何霖, 田立丰, 周勇为

College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China

收稿日期:2012-04-30 修回日期:2012-09-05 出版日期:2012-12-01 发布日期:2012-12-01
基金资助:
Project supported by the National Basic Research Program of China (Grant No. 2009 CB724100) and the National Natural Science Foundation of China (Grant No. 11172326).

Instantaneous and time-averaged flow structures around a blunt double-cone with or without supersonic film cooling visualized via nano-tracer planar laser scattering

Zhu Yang-Zhu (朱杨柱), Yi Shi-He (易仕和), He Lin (何霖), Tian Li-Feng (田立丰), Zhou Yong-Wei (周勇为)

College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China

Received:2012-04-30 Revised:2012-09-05 Online:2012-12-01 Published:2012-12-01
Contact: Yi Shi-He E-mail:ysh_1819@yahoo.com.cn
Supported by:
Project supported by the National Basic Research Program of China (Grant No. 2009 CB724100) and the National Natural Science Foundation of China (Grant No. 11172326).

摘要/Abstract

摘要： In a Mach 3.8 wind tunnel, both instantaneous and time-averaged flow structures of different scales around a blunt double-cone with or without supersonic film cooling were visualized via nano-tracer planar laser scattering (NPLS), which has a high spatiotemporal resolution. Three experimental cases with different injection mass flux rates were carried out. Lots of typical flow structures were clearly shown, such as shock wave, expansion fan, shear layer, mixing layer, and turbulent boundary layer. The analysis of two NPLS images with an interval of 5 μs revealed the temporal evolution characteristics of flow structures. With matched pressures, the laminar length of the mixing layer was longer than that in the case with a larger mass flux rate, but the full covered region was shorter. Structures like K-H (Kelvin-Helmholtz) vortices were clearly seen in both flows. Without injection, the flow was similar to the supersonic flow over a backward-facing step, and the structures were relatively simpler, and there was a longer laminar region. Large scale structures such as hairpin vortices were visualized. In addition, the results were compared in part with the schlieren images captured by others under the similar conditions.

关键词: blunt cone, supersonic flow structure, flow visualization, supersonic film cooling

Abstract: In a Mach 3.8 wind tunnel, both instantaneous and time-averaged flow structures of different scales around a blunt double-cone with or without supersonic film cooling were visualized via nano-tracer planar laser scattering (NPLS), which has a high spatiotemporal resolution. Three experimental cases with different injection mass flux rates were carried out. Lots of typical flow structures were clearly shown, such as shock wave, expansion fan, shear layer, mixing layer, and turbulent boundary layer. The analysis of two NPLS images with an interval of 5 μs revealed the temporal evolution characteristics of flow structures. With matched pressures, the laminar length of the mixing layer was longer than that in the case with a larger mass flux rate, but the full covered region was shorter. Structures like K-H (Kelvin-Helmholtz) vortices were clearly seen in both flows. Without injection, the flow was similar to the supersonic flow over a backward-facing step, and the structures were relatively simpler, and there was a longer laminar region. Large scale structures such as hairpin vortices were visualized. In addition, the results were compared in part with the schlieren images captured by others under the similar conditions.

Key words: blunt cone, supersonic flow structure, flow visualization, supersonic film cooling

中图分类号: (Supersonic and hypersonic flows)

47.40.Ki

47.80.Jk (Flow visualization and imaging) 47.40.-x (Compressible flows; shock waves) 47.80.-v (Instrumentation and measurement methods in fluid dynamics)

朱杨柱, 易仕和, 何霖, 田立丰, 周勇为. Instantaneous and time-averaged flow structures around a blunt double-cone with or without supersonic film cooling visualized via nano-tracer planar laser scattering[J]. Chin. Phys. B, 2013, 22(1): 14702-014702.

Zhu Yang-Zhu (朱杨柱), Yi Shi-He (易仕和), He Lin (何霖), Tian Li-Feng (田立丰), Zhou Yong-Wei (周勇为). Instantaneous and time-averaged flow structures around a blunt double-cone with or without supersonic film cooling visualized via nano-tracer planar laser scattering[J]. Chin. Phys. B, 2013, 22(1): 14702-014702.

参考文献 35

[1]	Li G C 2006 Aero-optics (Beijing: National Defense Industry Press) pp. 12-17 (in Chinese)
[2]	Eckert E R G 1952 Heat-Transfer Symposium, Michigan, American p. 195
[3]	Seban R A and Back L H 1962 Journal of Heat Transfer 84 45
[4]	Daanish M, Krian D and Christopher C 2010 AIAA Paper 2010-6886
[5]	Aupoix B, Mignosi A, Viala S, Bouvier F and Gaillard R 1998 AIAA Paper 96-0657
[6]	Mark A and Roy J 1993 AIAA Paper 93-2442
[7]	Juhany K A, Hunt M L and Sivo J M 1994 Journal of Thermophysics and Heat Transfer 8 59
[8]	Singh M, Singh L P and Husain A 2011 Chin. Phys. Lett. 28 094701
[9]	Singh L P, Husain A and Singh M 2010 Chin. Phys. Lett. 27 014702
[10]	Wang L and Lu X Y 2011 Chin. Phys. Lett. 28 064702
[11]	Cao Y H, Pei J, Chen J and She Z S 2008 Chin. Phys. Lett. 25 3315
[12]	Xu J L and Ma H Y 2007 Chin. Phys. Lett. 24 763
[13]	Lian Q X and Guo H 2004 Acta Phys. Sin. 53 2226 (in Chinese)
[14]	Zhao D M and Zhang Q C 2010 Chin. Phys. B 19 030518
[15]	Liu S L, Zhang L M, Chen C X, Ma X X and Zhu N L 1995 Acta Phys. Sin. B 44 825
[16]	Li S H, Liu B C, Ni G Q and Xu Z Z 2003 Chin. Phys. B 12 0856
[17]	Jiang S E, Yang J M, Zheng Z J and Ding Y K 2007 Chin. Phys. B 16 0193
[18]	Meyer T R 2002 Exp. in Fluids 32 603
[19]	Elliott G S, Glumac N and Carter C D 1999 AIAA Paper 99-0643
[20]	Fu P T, Han J F, Mou Y H, Han D and Yang C W 2011 Acta Phys. Sin. 60 053602 (in Chinese)
[21]	Gao Q, Yi S H, Jiang Z F, Zhao Y X and Xie W K 2012 Chin. Phys. B 21 064701
[22]	Han J and Jiang N 2008 Chin. Phys. Lett. 25 1731
[23]	Zhao Y X, Yi S H, Tian L F and Cheng Z Y 2009 Sci. China Ser. E 52 3640
[24]	Zhao Y X, Yi S H, He L, Cheng Z Y and Tian L F 2007 Chin. Sci. Bull. 52 1297
[25]	Zhao Y X, Yi S H, He L, Cheng Z Y and Tian L F 2007 Journal of National University of Defense Technology 29 12 (in Chinese)
[26]	Zhao Y X, Yi S H, Tian L F, He L and Cheng Z Y 2008 Sci. China Ser. G 51 1134
[27]	Yi S H, He L, Zhao Y X, Tian L F and Cheng Z Y 2009 Sci. China Ser. G 52 2001
[28]	He L, Yi S H, Zhao Y X, Tian L F and Chen Z 2011 Chin. Sci. Bull. 56 489
[29]	Yang W B, Zhuang F G, Shen Q, Guan F M, Wang Q, Yi S H, Zhao Y X, He L and Tian L F 2009 Sci. China Ser. G 52 1624
[30]	Hornak J P 2002 Encyclopedia of Imaging Science and Technology (New York: John Wiley and Sons) p. 390
[31]	Chen Z, Yi S H, Tian L F, He L and Zhu Y Z 2012 Shock Waves (published online)
[32]	Tian L F, Yi S H, Zhao Y X, He L and Cheng Z Y 2009 Sci. China Ser. G 52 1357
[33]	Maqbool D 2010 Development of an Experiment for Measuring Film Cooling Performance in Supersonic Flows (M. S. thesis) (College Park: the University of Maryland)
[34]	Chen Z, Yi S H and He L 2012 Chin. Sci. Bull. 57 584
[35]	Pedersen D, Eckert E and Goldstein R 1977 Journal of Heat Transfer 99 620

Instantaneous and time-averaged flow structures around a blunt double-cone with or without supersonic film cooling visualized via nano-tracer planar laser scattering

Instantaneous and time-averaged flow structures around a blunt double-cone with or without supersonic film cooling visualized via nano-tracer planar laser scattering

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