Review of research on the receptivity of hypersonic boundary layer

Jiang Xianyang; Li Cunbiao

doi:10.11729/syltlx20160129

Volume 31 Issue 2

Turn off MathJax

Article Contents

Article Navigation > Journal of Experiments in Fluid Mechanics > 2017 > 31(2): 1-11

Jiang Xianyang, Li Cunbiao. Review of research on the receptivity of hypersonic boundary layer[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(2): 1-11. doi: 10.11729/syltlx20160129

Citation:

Jiang Xianyang, Li Cunbiao. Review of research on the receptivity of hypersonic boundary layer[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(2): 1-11. doi: 10.11729/syltlx20160129

Citation:

Jiang Xianyang, Li Cunbiao. Review of research on the receptivity of hypersonic boundary layer[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(2): 1-11. doi: 10.11729/syltlx20160129

PDF( 7434 KB)

Review of research on the receptivity of hypersonic boundary layer

doi: 10.11729/syltlx20160129

Jiang Xianyang^1
,,
Li Cunbiao^{1, 2
,
,}

1.
State Key Laboratory for Turbulence and Complex System, College of Engineering, Peking University, Beijing 100871, China
2.
Collaborative Innovation Center of Advanced Aero-Engines, Beijing 100191, China

Received Date: 2016-09-02
Rev Recd Date: 2016-10-26
Publish Date: 2017-04-25

Abstract

Abstract

As a key aspect of transition prediction and control, receptivity process in hypersonic boundary layer is of great importance. However, it still has not been thoroughly understood, and is especially lacking in experimental verification. In this paper, two categories of disturbances are reviewed, namely, free-stream disturbance (acoustic, vertical, thermal perturbation, shock wave and particulates) and wall-induced disturbances (roughness, vibration, blowing and suction, surface heating and cooling). Mostly concerned are the theory of Fedorov about leading-edge receptivity and inter-modal exchange mechanism. In order to make the issue of receptivity more clearly understood, a compendious path diagram is sketched to describe paths to Mack modes.
- hypersonic boundary layer,
- receptivity,
- review,
- theory research,
- acoustic,
- roughness,
- wall temperature

FullText(HTML)

References(84)

References

[1]	Schmid P J, Henningson D S. Stability and transition in shear flows[M]. New York:Springer-Verlag, 2001.
[2]	Morkovin M V. Bypass transition to turbulence and research desiderata[R]. NASA Lewis Research Center Transition in Turbines, 1985.
[3]	Durbin P, Wu X. Transition beneath vortical disturbances[J]. Annual Review of Fluid Mechanics, 2007, 39(1):107-128. doi: 10.1146/annurev.fluid.39.050905.110135
[4]	Kachanov Y S. Physical mechanisms of laminar-boundary-layer transition[J]. Annual Review of Fluid Mechanics, 1994, 26(1):411-482. doi: 10.1146/annurev.fl.26.010194.002211
[5]	Lee C B, Wu J Z. Transition in wall-bounded flows[J]. Applied Mechanics Reviews, 2008, 61(3):030802. doi: 10.1115/1.2909605
[6]	Mack L M. Boundary-layer stability theory[R]. AGRAD-R-709, 1984.
[7]	Stetson K, Thompson E, Donaldson J, et al. Laminar boundary layer stability experiments on a cone at Mach 8. Ⅴ-tests with a cooled model[R]. AIAA-89-1895, 1989.
[8]	Stetson K, Thompson E, Donaldson J, et al. Laminar boundary layer stability experiments on a cone at Mach 8. Ⅰ-Sharp cone[C]. 16th Fluid and Plasmadynamics Conference, Massachusetts, 1983.
[9]	Stetson K, Thompson E, Donaldson J, et al. Laminar boundary layer stability experiments on a cone at Mach 8. Ⅱ-Blunt cone[C]. 22nd Aerospace Sciences Meeting, 1984.
[10]	Stetson K, Thompson E, Donaldson J, et al. Laminar boundary layer stability experiments on a cone at Mach 8. Ⅲ-Sharp cone at angle of attack[C]. 23rd Aerospace Sciences Meeting, 1985.
[11]	Stetson K, Thompson E, Donaldson J, et al. Laminar boundary layer stability experiments on a cone at Mach 8. Ⅳ-On unit Reynolds number and environmental effects[C]. 4th Joint Fluid Mechanics, Plasma Dynamics and Lasers Conference, 1986.
[12]	Bountin D, Sidorenko A, Shiplyuk A. Development of natural disturbances in a hypersonic boundary layer on a sharp cone[J]. Journal of Applied Mechanics and Technical Physics, 2001, 42(1):57-62. doi: 10.1023/A:1018852410488
[13]	Dong M, Luo J S. Mechanism of transition in a hypersonic sharp cone boundary layer with zero angle of attack[J]. Applied Mathematics and Mechanics, 2007, 28(8):1019-1028. doi: 10.1007/s10483-007-0804-2
[14]	Pruett C D, Chang C L. Direct numerical simulation of hypersonic boundary-layer flow on a flared cone[J]. Theoretical and Computational Fluid Dynamics, 1998, 11(1):49-67. doi: 10.1007/s001620050080
[15]	Fezer A, Kloker M. Spatial direct numerical simulation of transition phenomena in supersonic flat-plate boundary layers[M]. Springer Berlin Heidelberg, 2000.
[16]	Reshotko E. Boundary-layer stability and transition[J]. Annual Review of Fluid Mechanics, 1976, 8(1):311-349.
[17]	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. http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201501027.htm Luo J S. Transition and prediction for hypersonic boundary layers[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1):357-372. http://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201501027.htm
[18]	Fedorov A V, Khokhlov A P. Receptivity of hypersonic boundary layer to wall disturbances[J]. Theoretical and Computational Fluid Dynamics, 2002, 15(4):231-254. doi: 10.1007/s001620100052
[19]	Westin K J A, Bakchinov A A, Kozlov V V, et al. Experiments on localized disturbances in a flat plate boundary layer. Part 1. The receptivity and evolution of a localized free stream disturbance[J]. European Journal of Mechanics B-Fluids, 1998, 17(6):823-846. doi: 10.1016/S0997-7546(99)80016-8
[20]	Borodulin V I, Ivanov A V, Kachanov Y S, et al. Receptivity coefficients at excitation of cross-flow waves by free-stream vortices in the presence of surface roughness[J]. Journal of Fluid Mechanics, 2013, 716:487-527. doi: 10.1017/jfm.2012.555
[21]	Saric W S, Reed H L, Kerschen E J. Boundary-layer receptivity to freestream disturbances[J]. Annual Review of Fluid Mechanics, 2002, 34:291-319.
[22]	Zhong X L, Wang X W. Direct numerical simulation on the receptivity, instability, and transition of hypersonic boundary layers[J]. Annual Review of Fluid Mechanics, 2012, 44:527-561. doi: 10.1146/annurev-fluid-120710-101208
[23]	Fedorov A V. Transition and stability of high-speed boundary layers[J]. Annual Review of Fluid Mechanics, 2011, 43(1):79-95. doi: 10.1146/annurev-fluid-122109-160750
[24]	Balakumar P. Receptivity of hypersonic boundary layers to acoustic and vortical disturbances (invited)[C]. 45th AIAA Fluid Dynamics Conference, 2015.
[25]	McKenzie J F, Westphal K O. Interaction of linear waves with oblique shock waves[J]. Physics of Fluids, 1968, 11(11):2350-2362. doi: 10.1063/1.1691825
[26]	Ma Y B, Zhong X L. Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound[J]. Journal of Fluid Mechanics, 2003, 488:79-121. doi: 10.1017/S0022112003004798
[27]	Fedorov A V, Khokhlov A P. Excitation of unstable modes in a supersonic boundary layer by acoustic waves[J]. Fluid Dyna-mics, 1991, 26(4):531-537.
[28]	Fedorov A V, Khokhlov A P. Excitation and evolution of unstable disturbances in supersonic boundary layer[C]. Proceedings of ASME Fluid Engineering Conference, 1993, 151:1-13.
[29]	Fedorov A V, Tumin A. Initial value problem for hypersonic boundary layer flows[C]. 15th AIAA Computational Fluid Dynamics Conference, 2001.
[30]	Herbert T, Lin N A Y. Studies of boundary-layer receptivity with parabolized stability equations[C]. 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference, 1993.
[31]	Maslov A A, Shiplyuk A N, Sidorenko A A, et al. Leading-edge receptivity of a hypersonic boundary layer on a flat plate[J]. Journal of Fluid Mechanics, 2001, 426:73-94. doi: 10.1017/S0022112000002147
[32]	Schneider S P. Development of hypersonic quiet tunnels[J]. Journal of Spacecraft & Rockets, 2008, 45(45):641-664.
[33]	张传鸿. 高超声速静风洞的调试及圆锥边界层转捩的实验研究[D]. 北京: 北京大学, 2014. Zhang C H. The development of hypersonic quiet wind tunnel and experimental investigation of hypersonic boundary-layer transition on a flared cone[D]. Beijing:Peking University, 2014.
[34]	Zhang C, Lee C. Rayleigh-scattering visualization of the deve-lopment of second-mode waves[J]. Journal of Visualization, 2016:1-6.
[35]	Fedorov A V, Khokhlov A P. Sensitivity of a supersonic boundary layer to acoustic disturbances[J]. Fluid Dynamics, 1992, 27(1):29-34. doi: 10.1007/BF01054169
[36]	Fedorov A V, Khokhlov A P, Khokhlov P. Prehistory of instability in a hypersonic boundary layer[J]. Theoretical and Computational Fluid Dynamics, 2001, 14(6):359-375. doi: 10.1007/s001620100038
[37]	Ma Y B, Zhong X L. Numerical simulation of receptivity and stability of nonequilibrium reacting hypersonic boundary layers[C]. 39th Aerospace Sciences Meeting and Exhibit, 2001.
[38]	Fedorov A V. Receptivity of a high-speed boundary layer to acoustic disturbances[J]. Journal of Fluid Mechanics, 2003, 491:101-129. doi: 10.1017/S0022112003005263
[39]	Fedorov A V, Tumin A. Initial-value problem for hypersonic boundary-layer flows[J]. AIAA Journal, 2003, 41(3):379-389. doi: 10.2514/2.1988
[40]	Ma Y B, Zhong X L. Receptivity of a supersonic boundary layer over a flat plate. Part 1:Wave structures and interactions[J]. Journal of Fluid Mechanics, 2003, 488:31-78. doi: 10.1017/S0022112003004786
[41]	周恒, 苏彩虹, 张永明.超声速/高超声速边界层的转捩机理及预测[M].北京:科学出版社, 2015. Zhou H, Su C H, Zhang Y M. Transition mechanism and prediction of supersonic/hypersonic boundary layers[M]. Beijing:Science Press, 2015.
[42]	Ma Y B, Zhong X L. Receptivity of a supersonic boundary layer over a flat plate. Part 3. Effects of different types of free-stream disturbances[J]. Journal of Fluid Mechanics, 2005, 532:63-109. doi: 10.1017/S0022112005003836
[43]	Gao J, Luo J S, Wu X S. Receptivity of hypersonic boundary layer due to fast-slow acoustics interaction[J]. Acta Mechanica Sinica, 2015, 31(6):899-909. doi: 10.1007/s10409-015-0504-8
[44]	张玉东, 傅德薰, 马延文, 等.钝锥高超声速边界层来流感受性数值研究[J].中国科学, 2008, 38(9):1246-1254. http://www.cnki.com.cn/Article/CJFDTOTAL-JGXK200809016.htm Zhang Y D, Fu D X, Ma Y W, et al. Receptivity to free-stream disturbance waves for hypersonic flow over a blunt cone[J]. Science in China, Series G:Physics, Mechanics and Astronomy, 2008, 38(9):1246-1254. http://www.cnki.com.cn/Article/CJFDTOTAL-JGXK200809016.htm
[45]	Shi J, Tang X, Wang Z, et al. Receptivity of boundary layer over a blunt wedge due to freestream pulse disturbances at Mach 6[J]. International Journal of Aerospace Engineering, 2016, (1):1-14.
[46]	Kara K, Balakumar P, Kandil O. Receptivity of hypersonic boundary layers due to acoustic disturbances over blunt cone[C]. AIAA Aerospace Sciences Meeting and Exhibit, 2007.
[47]	Balakumar P, Kegerise M A. Receptivity of hypersonic boundary layers over straight and flared cones[J]. AIAA Journal, 2015, 53(8):2097-2109. doi: 10.2514/1.J053432
[48]	Zhong X L, Lei J. Numerical simulation of nose bluntness effects on hypersonic boundary layer receptivity to freestream disturbances[R]. AIAA-2011-30379.
[49]	Potter J L. Review of the influence of cooled walls on boundary-layer transition[J]. AIAA Journal, 1980, 18(8):1010-1012. doi: 10.2514/3.7703
[50]	Stetson K F, Kimmel R L. Surface temperature effects on boundary-layer transition[J]. AIAA Journal, 1992, 30(11):2782-2783. doi: 10.2514/3.11300
[51]	Kara K, Balakumar P, Kandil O. Effects of wall cooling on hypersonic boundary layer receptivity over a cone[C]. 38th Fluid Dynamics Conference and Exhibit, 2008.
[52]	Blanchard A E. Investigation of wall-cooling effects on hypersonic boundary-layer stability in a quiet wind tunnel[D]. Norfolk, VA:Old Dominion University, 1995.
[53]	Demetriades A. New experiments on hypersonic boundary layer stability including wall temperature effects[C]//Proceedings of the 1978 Heat Transfer and Fluid Mechanics Institute, 1978:39-54.
[54]	Decarlo J P, Sanator R J, Torrillo D T. Hypersonic boundary-layer transition data for a cold-wall slender cone[J]. AIAA Journal, 1965, 3(4):758-760. doi: 10.2514/3.2969
[55]	Lysenko V I, Maslov A A. The effect of cooling on supersonic boundary-layer stability[J]. Journal of Fluid Mechanics, 1984, 147:39-52. doi: 10.1017/S002211208400197X
[56]	Sidorenko A, Gromyko Y, Bountin D, et al. Effect of the local wall cooling/heating on the hypersonic boundary layer stability and transition[J]. EUCASS Proceedings Series-Advances in AeroSpace Sciences, 2015, 7:549-568.
[57]	Polivanov B P, Gromyko Y, Sidorenko A, et al. Effects of local wall heating and cooling on hypersonic boundary-layer stability[C]. Proceedings of the Summer Program 2011, 2011.
[58]	Soudakov V, Egorov I, Fedorov A. Numerical simulation of receptivity of a hypersonic boundary layer over a surface with temperature jump[C]. ESA Special Publication, 2009, 659.
[59]	Fedorov A V, Ryzhov A A, Soudakov V G, et al. Receptivity of a high-speed boundary layer to temperature spottiness[J]. Journal of Fluid Mechanics, 2013, 722:533-553. doi: 10.1017/jfm.2013.111
[60]	Egorov I V, Sudakov V G, Fedorov A V. Numerical modeling of the stabilization of a supersonic flat-plate boundary layer by a porous coating[J]. Fluid Dynamics, 2006, 41(3):356-365. doi: 10.1007/s10697-006-0051-x
[61]	Fedorov A. Transition and stability of high-speed boundary layers[J]. Annual Review of Fluid Mechanics, 2011, 43(1):79-95. doi: 10.1146/annurev-fluid-122109-160750
[62]	Schmisseur J D, Schneider S P, Collicott S H. Supersonic boundary-layer response to optically generated freestream disturbances[J]. Experiments in Fluids, 2002, 33(2):225-232. doi: 10.1007/s00348-001-0392-5
[63]	Kosinov A D, Maslov A A, Shevelkov S G. Experiments on the stability of supersonic laminar boundary-layers[J]. Journal of Fluid Mechanics, 1990, 219:621-633. doi: 10.1017/S0022112090003111
[64]	Fedorov A V, Ryzhov A A, Soudakov V G, et al. Numerical simulation of the effect of local volume energy supply on high-speed boundary layer stability[J]. Computers & Fluids, 2014, 100:130-137. https://www.research.manchester.ac.uk/portal/en/publications/numerical-simulation-of-the-effect-of-local-volume-energy-supply-on-highspeed-boundary-layer-stability(df644230-a44b-4476-80bc-8f5268bcd348).html
[65]	Kuester M S, White E B. Roughness receptivity and shielding in a flat plate boundary layer[J]. Journal of Fluid Mechanics, 2015, 777:430-460. doi: 10.1017/jfm.2015.267
[66]	Balakumar P. Boundary layer receptivity due to roughness and freestream sound for supersonic flows over axisymmetric cones[C]. 38th Fluid Dynamics Conference and Exhibit, Seattle, Washington, 2008.
[67]	Iyer P S, Muppidi S, Mahesh K. Roughness-induced transition in high speed flows[C]. 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, 2011.
[68]	Reda D C. Review and synthesis of roughness-dominated transition correlations for reentry applications[J]. Journal of Spacecraft and Rockets, 2002, 39(2):161-167. doi: 10.2514/2.3803
[69]	Schneider S P. Effects of roughness on hypersonic boundary-layer transition[J]. Journal of Spacecraft and Rockets, 2008, 45(2):193-209. doi: 10.2514/1.29713
[70]	Schneider S P. Summary of hypersonic boundary-layer transition experiments on blunt bodies with roughness[J]. Journal of Spacecraft and Rockets, 2008, 45(6):1090-1105. doi: 10.2514/1.37431
[71]	Wang X, Zhong X. Receptivity of a hypersonic flat-plate boundary layer to three-dimensional surface roughness[J]. Journal of Spacecraft and Rockets, 2008, 45(6):1165-1175. doi: 10.2514/1.37766
[72]	Mistry V I, Page G J, McGuirk J J. Simulation of receptivity and induced transition from discrete roughness elements[J]. Flow, Turbulence and Combustion, 2015, 95(2):301-334. https://www.researchgate.net/profile/James_Mcguirk/publication/283166050_Simulation_of_Receptivity_and_Induced_Transition_From_Discrete_Roughness_Elements/links/563895db08ae51ccb3cc5a62.pdf
[73]	Tang Q, Zhu Y D, Chen X, et al. Development of second-mode instability in a Mach 6 flat plate boundary layer with two-dimensional roughness[J]. Physics of Fluids, 2015, 27(6):064105. doi: 10.1063/1.4922389
[74]	Egorov I V, Fedorov A V, Soudakov V G. Receptivity of a hypersonic boundary layer over a flat plate with a porous coating[J]. Journal of Fluid Mechanics, 2008, 601:165-187.
[75]	Duan L, Wang X W, Zhong X L. A high-order cut-cell method for numerical simulation of hypersonic boundary-layer instability with surface roughness[J]. Journal of Computational Phy-sics, 2010, 229(19):7207-7237. doi: 10.1016/j.jcp.2010.06.008
[76]	Fong K D, Wang X W, Huang Y T, et al. Second mode suppression in hypersonic boundary layer by roughness:design and experiments[J]. AIAA Journal, 2015, 53(10):3138-3143. doi: 10.2514/1.J054100
[77]	Balakumar P. Receptivity of hypersonic boundary layers to distributed roughness and acoustic disturbances[C]. 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2013.
[78]	Wang X W, Zhong X L. Effect of wall perturbations on the receptivity of a hypersonic boundary layer[J]. Physics of Fluids, 2009, 21(4):044101. doi: 10.1063/1.3103880
[79]	Ladd D M, Hendricks E W. The effect of background particulates on the delayed transition of a heated 9-1 ellipsoid[J]. Experiments in Fluids, 1985, 3(2):113-119. doi: 10.1007/BF00276718
[80]	Lauchle G C, Petrie H L, Stinebring D R. Laminar-flow performance of a heated body in particle-laden water[J]. Experiments in Fluids, 1995, 19(5):305-312. doi: 10.1007/BF00203414
[81]	Holden M S. Studies of transitional flow, unsteady separation phenomena and particle induced augmentation heating on ablated nose tips[R]. AFOSR-TR-76-1066, 1975.
[82]	Fedorov A V, Tumin A. High-speed boundary-layer instability:old terminology and a new framework[J]. AIAA Journal, 2011, 49(8):1647-1657. doi: 10.2514/1.J050835
[83]	Van Ingen J L. The e^N method for transition prediction:historical review of work at TU delft[C]. 38th Fluid Dynamics Conference and Exhibit, 2008.
[84]	Lau K Y. Hypersonic boundary-layer transition:application to high-speed vehicle design[J]. Journal of Spacecraft and Rockets, 2008, 45(2):176-183. doi: 10.2514/1.31134