[1] Schneider S P, Juliano T J, Hannon M. Laminar-turbulent transition measurements in the Boeing/AFOSR Mach-6 quiet tunnel,AIAA-2007-4489[R]. Reston: AIAA, 2007.[2] Laufer J, Vrebalovich T. Stability and transition of a supersonic laminar boundary layer on an insulated at plate[J]. Journal of Fluid Mechanics, 1960(9): 257-299.[3] Blanchard A E, Selby G V. An experimental investigation of wall-cooling effects on hypersonic boundary-layer stability in a quiet wind tunnel, NASA-CR-198287[R]. Washington, D.C.: NASA, 1996.[4] Yi S H, Tian L F, Zhao Y X, et al. The new advance of the experimental research on compressible turbulence based on the NPLS technique[J]. Advance in Mechanics, 2011, 41(4): 379-390(in Chinese). 易仕和, 田立丰, 赵玉新, 等. 基于NPLS技术的可压缩湍流机理实验研究新进展[J]. 力学进展, 2011, 41(4): 379-390.[5] Yi S H, He L, Tian L F, et al. The application of nano-tracer planar laser scattering in shock wave field measurement[J]. Advance in Mechanics, 2012, 42(2): 197-205(in Chinese). 易仕和, 何霖, 田立丰, 等. 纳米示踪平面激光散射技术在激波复杂流场测量中的应用[J]. 力学进展, 2012, 42(2): 197-205.[6] Chen Z. Turbulent structure measurements and the relative technique researches of supersonic flow over a backward facing step[D]. Changsha: National University of Defense Technology, 2010 (in Chinese). 陈植. 超声速后台阶湍流结构试验及其相关技术研究[D]. 长沙: 国防科学技术大学, 2010.[7] Zhao Y X, Yi S H, Tian L F. Supersonic flow imaging via nanoparticles[J]. Science in China Series E: Technological Sciences, 2009, 52(12): 3640-3648.[8] Zhao Y X. Experimental investigation of spatiotemporal structures of supersonic mixing layer[D]. Changsha: National University of Defence Technology, 2008 (in Chinese). 赵玉新. 超声速混合层时空结构的实验研究[D]. 长沙: 国防科学技术大学, 2008.[9] Tian L F, Yi S H, Zhao Y X. Study of density field measurement based on NPLS technique in supersonic flow[J]. Science in China Series G: Physics, Mechanics & Astronomy, 2009, 52(9): 1357-1363.[10] Chen Z, Yi S H, Zhou Y W. Design of a hypersonic quiet wind tunnel nozzle based the throat boundary layer suction[C]//Proceedings of the 14th Chinese National Symposium on Shock Waves. Huangshan: [s.n.], 2010: 443-448(in Chinese). 陈植, 易仕和, 周勇为. 基于喉部边界层抽吸高超声速静风洞喷管设计[C]//第十四届全国激波与激波管学术会议.黄山: [s.n.], 2010: 443-448.[11] He L, Yi S H, Zhao Y X, et al. Experimental study of a supersonic turbulent boundary layer using PIV[J]. Science in China Series G: Physics, Mechanics & Astronomy, 2011, 54(9): 1702-1709.[12] He L, Yi S H, Zhao Y X, et al. Visualization of coherent structures in a supersonic flat-plate boundary layer[J]. Chinese Science Bulletin, 2011, 56(6): 489-494.[13] He L. Experimental investigation of supersonic boundary layer and shock wave/boundary layer interaction[D]. Changsha: National University of Defense Technology, 2011 (in Chinese). 何霖. 超声速边界层及激波与边界层相互作用的实验研究[D]. 长沙: 国防科学技术大学, 2011.[14] Zhao Y X, Tian L F, Yi S H. Experimental study of flow structure in pressure unmatched mixing layer[J]. Journal of Experiments in Fluid Mechanics, 2007, 21(3): 14-17.[15] Zhao Y X, Yi S H, Tian L F. The quantificational measurement of supersonic mixing layer growth rate[J]. Journal of Experiments in Fluid Mechanics, 2009, 23(3): 100-103.[16] Zhao Y X, Yi S H, He L. The fractal measurement of experimental images of supersonic turbulent mixing layer[J]. Science in China Series G: Physics, Mechanics & Astronomy, 2008, 51(8): 1134-1143.[17] Zhao Y X, Yi S H, He L. The experimental research of shocklet in supersonic turbulent mix layer[J]. Journal of National University of Defense Technology, 2007, 29(1): 12-15.[18] Zhao Y X, Yi S H, He L. The experimental study of interaction between shock wave and turbulence[J]. Chinese Science Bulletin, 2007, 52(10): 1297-1301.[19] Yi S H, He L, Zhao Y X. A flow control study of a supersonic mixing layer via NPLS[J]. Science in China Series G: Physics, Mechanics & Astronomy, 2009, 52(12): 2001-2006.[20] Zhao Y X, Yi S H, Tian L F. Multiresolution analysis of density fluctuation in supersonic mixing layer[J]. Science in China Series E: Technological Sciences, 2010, 53(2): 584-591.[21] Yi S H, He L, Tian L F, et al. Progress and prospect of the experimental researches on supersonic turbulent mechanism[C]//Proceedings of the 14th Chinese National Symposium on Shock Waves. Huangshan: [s.n.], 2010: 29-43(in Chinese). 易仕和, 何霖, 田立丰, 等. 超声速湍流机理实验研究—进展与展望[C]//第十四届全国激波与激波管学术会议. 黄山: [s.n.], 2010: 29-43.[22] Wu Y, Yi S H, Chen Z, et al. Experimental investigations on structures of supersonic laminar/turbulent flow over a compression ramp[J]. Acta Physica Sinica, 2013, 62(18): 184702 (in Chinese) 武宇, 易仕和, 陈植, 等. 超声速层流/湍流压缩拐角流动结构的实验研究[J]. 物理学报, 2013, 62(18): 184702.[23] Quan P C, Yi S H, Wu Y, et al. Experimental investigation of interactions between laminar or turbulent boundary layer and shock wave[J]. Acta Physica Sinica, 2014, 63(8): 084703 (in Chinese). 全鹏程, 易仕和, 武宇, 等. 激波与层流/湍流边界层相互作用实验研究[J]. 物理学报, 2014, 63(8): 084703.[24] Li G C. Aero-optics[M]. Beijing: National Defence Industry Press, 2006 (in Chinese). 李桂春. 气动光学[M]. 北京: 国防工业出版社, 2006.[25] Neal D R, Copland J, Neal D. Shack-Hartmann wavefront sensor precision and accuracy[C]//Proceedings of SPIE, Angela Duparr Bhanwar Singh Seattle. 2002: 148-160.[26] Jumper E J, Fitzgerald E J. Recent advances in aero-optics[J]. Progress in Aerospace Sciences, 2001, 37(3): 299-339.[27] Sourgen F, Haertig J, Rey C. Comparison between background oriented schlieren measurements (B.O.S.) and numerical simulations, AIAA-2004-2602[R]. Reston: AIAA, 2004.[28] Yi S H, Tian L F, Zhao Y X. Aero-optical aberration measuring method based on NPLS and its application[J]. Chinese Science Bulletin, 2010, 55(31): 3545-3549.[29] Zhao Y X, Yi S H, Tian L F, et al. An experimental study of aero-optical aberration and dithering of supersonic mixing layer via BOS[J]. Science in China Series G: Physics, Mechanics & Astronomy, 2010, 53(1): 81-94.[30] Yi S H, Hou Z X, Zhao Y X. The optimization study of optical performance of shear layer in free-vortex ADW[J]. Experiments and Measurements in Fluid Mechanics, 2004, 18(2): 47-49 (in Chinese). 易仕和, 侯中喜, 赵玉新. 超声速自由涡气动窗口剪切层光学性能的优化设计研究[J]. 流体力学实验与测量, 2004, 18(2): 47-49.[31] Tian L F, Yi S H, Zhao Y X, et al. Aero-optical wave front measurement technique based on BOS and its applications[J]. Chinese Science Bulletin, 2011, 56(22): 2320-2326.[32] Zhao Y X, Yi S H, Tian L F, et al. Density field measurement and approximate reconstruction of supersonic mixing layer[J]. Chinese Science Bulletin, 2010, 55(19): 2004-2009.[33] Tian L F, Yi S H, Zhao Y X. PIV study of supersonic flow around an optical bow cap[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(1): 26-29.[34] Tian L F, Yi S H, Zhao Y X. Flow visualization of supersonic flow around a concave optical bow cap model[J]. Journal of Experiments in Fluid Mechanics, 2009, 23(1): 15-17. |