[1] [1] FAGE A，SARGENT R F. Shock wave and boundary layer phenomena near a flat surface[J]. Proc Roy Soc A，1947，190: 1-20.

[2] [2] LIEPMANN HW. The interaction between boundary layer and shock waves in transonic flow[J]. Journal of Aerospace Sciences，1946，13: 623-638.

[4] [4] TAN H，SUN S，YIN Z. Oscillatory flows of rectangular hypersonic inlet unstart caused by downstream massflow choking[J]. Journal of Propulsion and Power，2009，25（1）: 138-147.

[5] [5] MIYAZATO Y，IRIE M，YAMAMOTO H，et al. Quantitative flow visualization of correctly expanded supersonic jets by rainbow schlieren deflectometry[C]//AIAA paper，Wright-Patterson，USA: AIAA, 2013.

[6] [6] MASANORI O A K H. Computed- tomographic density measurement of supersonic flow field by colored- grid background oriented schlieren （CGBOS） technique[J].Measurement Science and Technology，2011，22（10）:104011.

[7] [7] YIP B，LYONS K，LONG M，et al. Visualization of a supersonic underexpanded jet by planar Rayleigh scattering[J]. Physics of Fluids A: Fluid Dynamics，1989，1（9）: 1449.

[8] [8] PANDA J，SEASHOLTZ R G. Measurement of shock structure and shock-vortex interaction in underexpanded jets using Rayleigh scattering[J]. Physics of Fluids，1999，11（12）: 3761-3777.

[10] [10] BOOKEY P，WYCKHAM C，SMITS A. Experimental investigations of Mach 3 shock wave turbulent boundary layer interactions[C]//Aiaa Fluid Dynamics Conference and Exhibit，San Diego, CA: AIAA, 2013.

[11] [11] SHELAR V M，MV S R，HEGDE G M，et al. Acetone planar laser-induced fluorescence for supersonic flow visualization in air and nitrogen jet[J]. International Journal of Mechanical and Materials Engineering，2014，9（1）: 28.

[12] [12] MAI T，SAKIMITSU Y，NAKAMURA H，et al. Effect of the incident shock wave interacting with transversal jet flow on the mixing and combustion[J]. Proceedings of the Combustion Institute，2011，33（2）: 2335-2342.

[13] [13] ROBINSON S K，SEEGMILLER M L，KUSSOY M I.Hot- wire and laser Doppler anemometer measurements in a supersonic boundary layer[J]. AIAA Paper，1983，83: 1723.

[14] [14] SMITS A J，DUSSAUGE J P. Turbulent shear layers in supersonic flow[M]. Springer，New York: 2006.

[15] [15] KOMIE H，BROSNAN S J，LITTON A B，et al. Realtime Doppler global velocimetry[C]//AIAA Paper，1991: 91-337.

[16] [16] KUHLMAN J. Development of Doppler global velocimeter（DGV）[R]. AFRL-SR-BL-TR-98-0494，1998.

[17] [17] WILLERT C，STOCKHAUSEN G，BEVERSDORFF M，et al. Application of Doppler global velocimetry in cryogenic wind tunnels[J]. Exp Fluids，2005，39: 420-430.

[18] [18] SAMIMY M，WERNET M P. Review of planar multiplecomponent velocimetry in high speed flows[J]. AIAA Journal，2000，38: 553-574.

[20] [20] SVIZHER A，COHEN J. Holographic particle image velocimetry system for measurements of hairpin vortices in air channel flow[J]. Exps Fluids，2006，40: 708-722.

[21] [21] TAO B，KATZ J，MENEVEAU C. Statistical geometry of sub grid scale stresses determined from holographic particle image velocimetry measurements[J]. J Fluid Mech，2002，457: 35-78.

[22] [22] HUMBLE R A，ELSINGA G E，SCARANO F，et al.Three- dimensional instantaneous structure of a shock wave/turbulent boundary layer interaction[J]. J Fluid Mech，2009，622: 33-62.

[23] [23] KIM K C，YOON S Y，KIM S M，et al. An orthogonalplane PIV technique for the investigations of three- dimensional vortical structures in a turbulent boundary layer flow[J]. Exps Fluids，2006，40: 876-883.

[26] [26] KRUGER S，GRUNEFELD G. Stereoscopic flow- tagging velocimetry[J]. Applied Physics B，1999，69（5）:509-512.

[27] [27] ISMAILOV M M，SCHOCK H J，FEDEWA A M. Gaseous flow measurements in an internal combustion engine assembly using molecular tagging velocimetry[J].Experiments in Fluids，2006，41（1）: 57-65.

[28] [28] RUBINSZTEIN D H，LITTLETON B，BARKER P，et al. Ionic strontium fluorescence as a method for flow tagging velocimetry[J]. Experiments in Fluids，2001，30（1）: 36-42.

[29] [29] SANCHEZ G R，SRINIVASAN R，BOWERSOX R D W，et al. Simultaneous velocity and temperature measurements in gaseous flow fields using the VENOM technique[J]. Optics Letters，2011，36（2）: 196-198.

[30] [30] PAN F，SANCHEZ G R，MCILVOYM H，et al. Simultaneous three-dimensional velocimetry and thermometry in gaseous flows using the stereoscopic vibrationally excited nitric oxide monitoring technique[J]. Optics Letters，2016，41（7）: 1376-1379.

[31] [31] RIBAROV L A，WEHREMYER J A，PITZ R W，et al.Hydroxyl tagging velocimetry （HTV） in experimental air flows[J]. Applied Physics B，2002，74（2）: 175-183.