Citation: | CHEN J F, XU Y, XU X B, et al. Pressure fluctuation experiments of hypersonic boundary-layer on a 7-degree half-angle sharp cone[J]. Journal of Experiments in Fluid Mechanics, 2023, 37(6): 51-60. DOI: 10.11729/syltlx20210054 |
[1] |
罗纪生. 高超声速边界层的转捩及预测[J]. 航空学报, 2015, 36(1): 357–372.
LUO J S. Transition and prediction for hypersonic boundary layers[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1): 357–372.
|
[2] |
SMITH F T. On the first-mode instability in subsonic, supersonic or hypersonic boundary layers[J]. Journal of Fluid Mechanics, 1989, 198: 127–153. doi: 10.1017/s0022112089000078
|
[3] |
MACK L M. Linear stability theory and the problem of supersonic boundary-layer transition[J]. AIAA Journal, 1975, 13(3): 278–289. doi: 10.2514/3.49693
|
[4] |
MACK L M. Boundary-layer linear stability theory[R]. AGARD Report 709, 1984.
|
[5] |
SARIC W S, Reed H L. Crossflow instabilities - theory & technology[R]. AIAA 2003-771, 2003. doi: 10.2514/6.2003-771
|
[6] |
SARIC W S. Görtler vortices[J]. Annual Review of Fluid Mechanics, 1994, 26(1): 379–409. doi: 10.1146/annurev.fl.26.010194.002115
|
[7] |
刘向宏, 赖光伟, 吴杰. 高超声速边界层转捩实验综述[J]. 空气动力学学报, 2018, 36(2): 196–212. DOI: 10.7638/kqdlxxb-2018.0017
LIU X H, LAI G W, WU J. Boundary-layer transition experiments in hypersonic flow[J]. Acta Aerodynamica Sinica, 2018, 36(2): 196–212. doi: 10.7638/kqdlxxb-2018.0017
|
[8] |
SCHMISSEUR J D. Hypersonics into the 21st century: a perspective on AFOSR-sponsored research in aerothermo-dynamics[J]. Progress in Aerospace Sciences, 2015, 72: 3–16. doi: 10.1016/j.paerosci.2014.09.009
|
[9] |
沈清, 袁湘江, 王强, 等. 可压缩边界层与混合层失稳结构的研究进展及其工程应用[J]. 力学进展, 2012, 42(3): 252–261.
SHEN Q, YUAN X J, WANG Q, et al. Review on the instability structure in compressible boundary layers and mixing layers and its application[J]. Advances in Mecha-nics, 2012, 42(3): 252–261.
|
[10] |
MUIR J, TRUJILLO A. Experimental investigation of the effects of nose bluntness, free-stream unit Reynolds number, and angle of attack on cone boundary layer transition at a Mach number of 6[C]//Proc of the 10th Aerospace Sciences Meeting. 1972. doi: 10.2514/6.1972-216
|
[11] |
STETSON K F, RUSHTON G H. Shock tunnel investiga-tion of boundary-layer transition at M = 5.5[J]. AIAA Journal, 1967, 5(5): 899–906. doi: 10.2514/3.4098
|
[12] |
JULIANO T J, KIMMEL R L, WILLEMS S, et al. HIFiRE-1 boundary-layer transition: ground test results and stability analysis[R]. AIAA 2015-1736, 2015. doi: 10.2514/6.2015-1736
|
[13] |
WILLEMS S, GUELHAN A, JULIANO T J, et al. Laminar to turbulent transition on the HIFiRE-1 cone at Mach 7 and high angle of attack[R]. AIAA 2014-0428, 2014. doi: 10.2514/6.2014-0428
|
[14] |
JULIANO T J, KIMMEL R L, WILLEMS S, et al. HIFiRE-1 surface pressure fluctuations from high Reynolds, high angle ground test[R]. AIAA 2014-0429, 2014. doi: 10.2514/6.2014-0429
|
[15] |
STETSON K F, THOMPSON E R, DONALDSON J C, et al. Laminar boundary layer stability experiments on a cone at Mach 8, part 1: sharp cone[R]. AIAA-83-1761, 1983.
|
[16] |
CASPER K M, BERESH S J, HENFLING J F, et al. Hypersonic wind-tunnel measurements of boundary-layer transition on a slender cone[J]. AIAA Journal, 2016, 54(4): 1250–1263. doi: 10.2514/1.j054033
|
[17] |
ZHANG C H, LEE C. Rayleigh-scattering visualization of the development of second-mode waves[J]. Journal of Visualization, 2017, 20(1): 7–12. doi: 10.1007/s12650-016-0384-4
|
[18] |
ZHU Y D, ZHANG C H, CHEN X, et al. Transition in hypersonic boundary layers: role of dilatational waves[J]. AIAA Journal, 2016, 54(10): 3039–3049. doi: 10.2514/1.j054702
|
[19] |
常雨, 陈苏宇, 张扣立. 高超声速边界层转捩特性试验探究[J]. 宇航学报, 2015, 36(11): 1318–1323. DOI: 10.3873/j.issn.1000-1328.2015.11.014
CHANG Y, CHEN S Y, ZHANG K L. Experimental investigation of hypersonic boundary layer transition[J]. Journal of Astronautics, 2015, 36(11): 1318–1323. doi: 10.3873/j.issn.1000-1328.2015.11.014
|
[20] |
LIU X L, YI S H, XU X W, et al. Experimental study of second-mode wave on a flared cone at Mach 6[J]. Physics of Fluids, 2019, 31(7): 074108. doi: 10.1063/1.5103192
|
[21] |
陈久芬, 凌岗, 张庆虎, 等. 7°尖锥高超声速边界层转捩红外测量实验[J]. 实验流体力学, 2020, 34(1): 60–66. DOI: 10.11729/syltlx20180172
CHEN J F, LING G, ZHANG Q H, et al. Infrared thermography experiments of hypersonic boundary-layer transition on a 7° half-angle sharp cone[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(1): 60–66. doi: 10.11729/syltlx20180172
|
[22] |
CHEN X, ZHU Y D, LEE C. Interactions between second mode and low-frequency waves in a hypersonic boundary layer[J]. Journal of Fluid Mechanics, 2017, 820: 693–735. doi: 10.1017/jfm.2017.233
|
1. |
屈东胜,樊宏杰,刘连伟,陈洁,邹前进. 基于近红外光谱的超声速燃烧场气体参数测量研究. 光学学报. 2020(03): 198-205 .
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