| [1] McGinley C B, Berry S A, Kinder G R, et al. Review of orbiter flight boundary layer transition data, AIAA-2006-2921[R]. Reston: AIAA, 2006.[2] Reshotko E. Transition issues at hypersonic speeds, AIAA-2006-0707[R]. Reston: AIAA, 2006.[3] 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, AIAA-1983-1761[R]. Reston: AIAA, 1983.[4] Stetson K F, Thompson E R, Donaldson J C, et al. Laminar boundary layer stability experiments on a cone at Mach 8, part 2: blunt cone, AIAA-1984-0006[R]. Reston: AIAA, 1984.[5] Stetson K F, Thompson E R, Donaldson J C, et al. Laminar boundary layer stability experiments on a cone at Mach 8, part 3: sharp cone at angle of attack, AIAA-1985-0492[R]. Reston: AIAA, 1985.[6] Stetson K F, Thompson E R, Donaldson J C, et al. Laminar boundary layer stability experiments on a cone at Mach 8, part4:on unit Reynolds number and environmental effects, AIAA-1986-1087[R]. Reston: AIAA, 1986.[7] Morkovin M V, Reshotko E, Herbert T. Transition in open flow systems a reassessment[J]. Bulletin of the American Physical Society, 1994, 39(9): 1882.[8] Morkovin M V. Critical evaluation of transition from laminar to turbulent shear layers with emphasis on hypersonically traveling bodies, AFFDL-TR-68-149[R]. Washington, D. C. : NASA, 1969.[9] Mack L M. Linear stability theory and the problem of supersonic boundary layer transition[J]. AIAA Journal, 1975, 13(3): 423-448.[10] Fedorov A V, Khokhlov A P. Excitation of unstable modes in a supersonic boundary layer by acoustic waves[J]. Fluid Dynamics, 1991, 26(4): 531-537.[11] Fedorov A V, Khokhlov A P. Excitation and evolution of unstable disturbances in supersonic boundary layer[C]//Proceedings of the ASME Fluids Engineering Conference. Vancouver: ASME Fluids Engineering Division, 1993, 151: 1-13.[12] Maslov A A, Shiplyuk A A, Sidorenko A A, et al. Leading edge receptivity of a hypersonic boundary layer on a flat plate[J]. Journal of Fluid Mechanics, 2001, 26(1):73-79.[13] Zhong X. Leading-edge receptivity to free stream disturbance waves for hypersonic flow over a parabola[J]. Journal of Fluid Mechanics, 2001, 441(16): 315-367.[14] Shen Q, Li Q, Deng X G, et al. Numerical simulation of two-dimensional hypersonic boundary layer stability, AIAA-1998-2484[R]. Reston: AIAA, 1998.[15] Zhang Y D, Fu D X, Ma Y W, et al. Numerical simulation of hypersonic boundary layer receptive on blunt cone[J]. SCIENCE CHINA Physics, Mechanics & Astronomy, 2008, 38(9): 1246-1254 (in Chinese). 张玉东, 傅徳薰, 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: 物理学 力学 天文学, 2008, 38(9): 1246-1254.[16] Mack L M. Boundary-layer stability theory, NASA-CR-131501[R]. Washington, D. C. : NASA, 1973.[17] Mack L M. Boundary-layer linear stability theory, AGARD 709 [R]. 1984.[18] Kendall J M. Supersonic boundary layer stability experiments, BSD-TR-67-213[R]. San Bernardino: Aerospace Corporation, 1967.[19] Kendall J M. Wind tunnel experiments relating to supersonic and hypersonic boundary layer transition[J]. AIAA Journal, 1975, 13(3): 290-299.[20] Ji F, Shen Q, Yuan X J, et al. Verification of direct numerical simulation on nypersonic boundary layer stability with LST[C]//The 11th Asian Congress of Fluid Mechanics. Malaysia: The Insitution of Engineers, 2006: 57.[21] Yan M, Luo J S. The bluntness effect on stability of boundary layer over blunt cone in supersonic flow[J]. Acta Aerodynamica Sinica, 2008, 26(4):430-434 (in Chinese). 闫溟, 罗纪生. 超声速流中圆锥头部钝度对边界层稳定性的影响[J]. 空气动力学学报, 2008, 26(4): 430-434.[22] Su C H, Zhou H. Stability analysis and transition prediction of hypersonic boundary layer over a blunt cone with small nose bluntness at zero angle of attack[J]. Applied Mathematics and Mechanics, 2007, 28(5): 505-513 (in Chinese). 苏彩虹, 周恒. 零攻角小钝头钝锥高超音速绕流边界层的稳定性分析和转捩预报[J]. 应用数学和力学, 2007, 28(5): 505-513.[23] Ji F, Guan F M, Shen Q, et al. An interferential streak instability of boundary layer over a cone at Mach 6, AIAA-2013-0255[R]. Reston: AIAA, 2013.[24] Zhong X L, Wang X W. Direct numerical simulation on the receptivity, instability, and transition of hypersonic boundary layers[J]. Annual Reviews of Fluid Mechanics, 2013, 44: 527-61.[25] Chokani N. Nonlinear spectral dynamics of hypersonic laminar boundary layer flow[J]. Physics of Fluids, 1999, 11(12): 3846-3851.[26] Shiplyuk A N, Bountin D A, Maslov A A, et al. Nonlinear mechanisms of the initial stage of the hypersonic boundary layer transition[J]. Journal of Applied Mechanics and Technical Physics, 2003, 44(5): 654-659.[27] Mayer C S J, Laible A C, Fasel H F. Numerical investigation of wave packets in a Mach 3.5 cone boundary layer[J]. AIAA Journal, 2011, 49(1): 67-86.[28] Sivasubramanian J, Fasel H F. Numerical investigation of boundary-layer transition initiated by a wave packet for a cone at Mach 6, AIAA-2010-0900[R]. Reston: AIAA, 2010.[29] Sivasubramanian J, Fasel H F. Transition initiated by a localized disturbance in a hypersonic flat-plate boundary layer, AIAA-2011-0374[R]. Reston: AIAA, 2011.[30] Sivasubramanian J, Fasel H F. Nonlinear stages of transition and breakdown in a boundary layer on a sharp cone at Mach 6, AIAA-2012-0087[R]. Reston: AIAA, 2012.[31] Ji F, Shen Q. Computation and analysis of hypersonic boundary layer stability[C]//The 1st Modern Aerodynamics and Aerothermodynamics Conference. Beijing: The Chinese Society of Theoretical and Applied Mechanics, 2006: 379-382 (in Chinese). 纪锋, 沈清. 高超声速边界层稳定性计算与分析[C]//中国第一届近代空气动力学与气动热力学会议论文集. 北京:中国空气动力学会, 2006: 379-382.[32] Berry S A, Nowak R J, Horvath T J. Boundary layer control for hypersonic airbreathing vehicles, AIAA-2004-2246[R]. Reston: AIAA, 2004.[33] Zhao J B, Shen Q, Zhang H J, et al. Boundary layer research of scramjet inlet based on the Tollmien-Schlichting(T-S) wave syntony[J]. Journal of Aerospace Power, 2010, 25(11): 2420-2424 (in Chinese). 赵俊波, 沈清, 张红军, 等. 基于T-S波谐频共振的超燃进气道边界层转捩[J]. 航空动力学报, 2010, 25(11): 2420-2424.[34] Zhang H J, Shen Q. Experimental studies of leading edge bluntness effects on hypersonic inlet[J]. Journal of Propulsion Technology, 2013, 34(10):1316-1320 (in Chinese). 张红军, 沈清. 高超声速进气道前缘钝度效应试验研究[J]. 推进技术, 2013, 34(10): 1316-1320. |
CJA
