[1] Sun Z X, Luo Y P, Li W J et al. Brief analysis of the development roadmap of American hypersonic weapons[J]. Tactical Missile Technology, 1-10(2023).

[2] Walker S, Sherk J, Shell D et al. The DARPA/AF falcon program: the hypersonic technology vehicle #2 (HTV-2) flight demonstration phase[C], 2539(2008).

[3] Dolvin D. Hypersonic international flight research and experimentation technology development and flight certification strategy[C], 7228(2009).

[4] Dolvin D. Hypersonic international flight research and experimentation (HIFiRE) fundamental science and technology development strategy[C], 2581(2008).

[5] Simmons J. Measurement techniques in high-enthalpy hypersonic facilities[J]. Experimental Thermal and Fluid Science, 10, 454-469(1995).

[6] Li Y. Research on non-contact optical measurement technology of flow field[D](2023).

[7] Zaplotnik R, Primc G, Vesel A. Optical emission spectroscopy as a diagnostic tool for characterization of atmospheric plasma jets[J]. Applied Sciences, 11, 2275(2021).

[8] Brandis A, Cruden B, Prabhu D et al. Analysis of air radiation measurements obtained in the EAST and X2 shocktube facilities[C], 4510(2010).

[9] Zeng H, Ou D B. Temperature measurements of inductively coupled plasma spheroidization by using argon emission spectroscopy[J]. Spectroscopy and Spectral Analysis, 40, 1685-1689(2020).

[10] Yan H, Zhang S H, Wang F Y et al. Measurement of high enthalpy gas flow temperature by NO laser-induced fluorescence[J]. Physics of Gases, 5, 1-7(2020).

[11] Seitzman J M, Kychakoff G, Hanson R K. Instantaneous temperature field measurements using planar laser-induced fluorescence[J]. Optics Letters, 10, 439-441(1985).

[12] Fraval E, Danehy P M, Houwing A F P. Single-shot broadband coherent anti-Stokes Raman scattering measurements in a free piston shock tunnel nozzle expansion[C], 22-27(2001).

[13] Roy S, Gord J R, Patnaik A K. Recent advances in coherent anti-Stokes Raman scattering spectroscopy: fundamental developments and applications in reacting flows[J]. Progress in Energy and Combustion Science, 36, 280-306(2010).

[14] Kan R F, Xia H H, Xu Z Y et al. Research and progress of flow field diagnosis based on laser absorption spectroscopy[J]. Chinese Journal of Lasers, 45, 0911005(2018).

[15] Eng R S, Butler J F, Linden K J. Tunable diode laser spectroscopy: an invited review[J]. Optical Engineering, 19, 945-960(1980).

[16] Werle P. A review of recent advances in semiconductor laser based gas monitors[J]. Spectrochimica Acta Part A: Molecular and Biomolecular Spectroscopy, 54, 197-236(1998).

[17] Ujager F S, Zaidi S M H, Younis U. A review of semiconductor lasers for optical communications[C], 107-111(2011).

[18] Parker R, Wakeman T, Holden M et al. Measuring nitric oxide freestream concentration using quantum cascade lasers at CUBRC[C], 926(2006).

[19] Weisberger J M, DesJardin P E, MacLean M et al. Near-surface carbon-dioxide tunable diode laser absorption spectroscopy concentration measurements in hypervelocity flow[J]. Journal of Spacecraft and Rockets, 52, 1551-1562(2015).

[20] Weisberger J M, MacLean M G, Parker R A et al. Near-surface nitric oxide concentration measurement in the LENS-XX expansion tunnel facility[C], 2643(2013).

[21] Hu S W, Yin K W, Tu X B et al. Measurement of CO concentration in flat flame based on mid-infrared absorption spectroscopy[J]. Journal of Experiments in Fluid Mechanics, 35, 60-66(2021).

[22] Wehe S, Baer D, Hanson R et al. Tunable diode-laser absorption measurements of temperature, velocity, and H2O in hypervelocity flows[C], 3267(1997).

[23] Chen W, Wu Y, Huang Z J et al. Monitoring copper species in flow of arc-heated wind tunnel based on TDLAS[J]. Acta Aeronautica et Astronautica Sinica, 40, 122841(2019).

[24] Ou D B, Chen L Z, Dong Y H et al. Measurements of gas temperature and atomic oxygen density in the arc-heated wind tunnel based on TDLAS[J]. Journal of Experiments in Fluid Mechanics, 29, 62-67(2015).

[25] Hanson R K, Spearrin R M, Goldenstein C S[M]. Spectroscopy and optical diagnostics for gases(2016).

[26] Jiang Z L. Theoretical innovation and engineering practice of Chinese hypervelocity wind tunnels[J]. Journal of Engineering Studies, 14, 469-482(2022).

[27] Lin Z B, Ge X Z, Yu X L et al. The nitric oxide concentration diagnostics in fuse stream of a high enthalpy shock tunnel[J]. Acta Mechanica Sinica, 33, 28-35(2001).

[28] Jiang Z L, Zhao W, Lin Z B et al. Research and development of detonation-driven high enthalpy shock wind tunnel and its transient testing technology[J]. Advances in Mechanics, 31, 312-317(2001).

[29] Yu X L, Yang Q S, Jiang N B et al. Measurement of nitric oxide concentration in a shock tunnel using absorptive spectroscopy technique[J]. Experiments and Measurements in Fluid Mechanics, 13, 62-66(1999).

[30] Lin Z B, Guo D H, Zhu N Y et al. The measurement and diagnostics in free stream of JF-10 hydrogen oxygen detonation driven shock tunnel[J]. Experiments and Measurements in Fluid Mechanics, 14, 12-17(2000).

[31] Li F, Yu X L, Chen L H et al. Temperature and water vapour concentration measurements of CH4/air premixed flat flame based on TDLAS[J]. Journal of Experiments in Fluid Mechanics, 23, 40-44(2009).

[32] Yu X L, Li F, Zhang S H et al. Diagnosis of supersonic flow using tunable diode laser absorption spectroscopy[C], 41(2009).

[33] Li F, Zhang X Y, Yu X L. Application of near-infrared absorption spectroscopy diagnostic technology in super-ignition research[D](2009).

[34] Li F, Yu X L, Lin X et al. Parallel-beam tomography based on TDLAS[J]. Chinese Journal of Theoretical and Applied Mechanics, 46, 54-59(2014).

[35] Zeng H, Yu X L, Li F et al. Nitric oxide concentration and temperature measurement for shock tunnel free stream using mid-infrared absorption spectroscopy[J]. Journal of Experiments in Fluid Mechanics, 29, 79-83(2015).

[36] Fang S H, Lin X, Yang J N et al. Experimental investigations of spectroscopic characteristics in high temperature interface on carbon-based composite materials[J]. Aerospace Technology, 159-169(2023).

[37] Xu Z Y, Kan R F, Ran J et al. A tunable diode laser absorption based velocity sensor for local field in hypersonic flows[C], ETu2A.4(2016).

[38] Zeng H, Chen L Z, Lin X et al. Laser absorption spectroscopy diagnostics in the arc-heater of an arcjet facility[J]. Journal of Experiments in Fluid Mechanics, 31, 28-33(2017).

[39] Lu H B, Chen X, Zeng X Z et al. Exploration of experimental techniques on Ma=10 scramjets in FD-21 high enthalpy shock tunnel[J]. Physics of Gases, 7, 1-12(2022).

[40] Lin J, Zhang T T, Song H Z et al. Flow field diagnosis and chamber parameters calculation method for arc heating high enthalpy wind tunnel[J]. Aerospace Technology, 52-59(2023).

[41] Song J L, Hong Y J, Wang G Y et al. Measurement of supersonic flow parameters using laser absorption spectroscopy[J]. Infrared and Laser Engineering, 43, 3510-3515(2014).

[42] Huang A, Zhao Y H, Yang S H et al. Temperature-measurement method based on boltzmann diagram for scramjet engine[J]. Chinese Journal of Lasers, 50, 1911004(2023).

[43] Xia H H, Zhang S P, Yang S H et al. Two-dimensional distribution measurement of scramjet engine direct-connected bench combustion field based on TDLAS multi-line absorption[J/OL]. Experimental Fluid Mechanics, 1-7. http://syltlx.com/cn/article/doi/10.11729/syltlx20220103

[44] Sun Z X, Li W J, Tang Z G et al. Analysis of aerodynamic ground test capability and development trend in the United States[J]. Acta Aerodynamica Sinica, 41, 1-21(2023).

[45] Sagnier P, Verant J L. Flow characterization in the ONERA F4 high-enthalpy wind tunnel[J]. AIAA Journal, 36, 522-531(1998).

[46] Sagnier P, Verant J L, Devezeaux D et al. Real gas flow characterization in the ONERA F4 high enthalpy wind tunnel[C], 378-388(2002).

[47] Mohamed A, Rosier B, Henry D et al. Tunable diode laser measurements on nitric oxide in a hypersonic wind tunnel[J]. AIAA Journal, 34, 494-499(1996).

[48] Arroyo M P, Langlois S, Hanson R K. Diode-laser absorption technique for simultaneous measurements of multiple gasdynamic parameters in high-speed flows containing water vapor[J]. Applied Optics, 33, 3296-3307(1994).

[49] Candler G V, Johnson H B, Nompelis I et al. Development of the US3D code for advanced compressible and reacting flow simulations[C], 1893(2015).

[50] Chaudhry R S, Boyd I D, Torres E et al. Implementation of a chemical kinetics model for hypersonic flows in air for high-performance CFD[C], 2191(2020).

[51] Boyd I D, Schwartzentruber T E[M]. Nonequilibrium gas dynamics and molecular simulation(2017).

[52] Lu H B, Chen X, Chen J M et al. Flight condition achievement of Mach number 8 in a new shock tunnel of CAAA and its scramjet experimental investigation[J]. Physics of Gases, 4, 13-24(2019).

[53] Ali Shams T, Ali Shah S I, Ahmad M A. Capability analysis of global hypersonic wind tunnel facilities for aerothermodynamic investigations[C], 481-501(2020).

[54] Berger K T, Hollingsworth K E, Wright S A et al. NASA langley aerothermodynamics laboratory: hypersonic testing capabilities[C], 1337(2015).

[55] Mills M. Hypersonic test capabilities in tunnels B and C at AEDC’s von karman facility[C], 1336(2015).

[56] Smith D M, Felderman E. Aerothermal testing of space and missile materials in the arnold engineering development center arc jet facilities[C](2006).

[57] Parker R, Wakeman T, MacLean M et al. Measuring nitric oxide freestream velocity using quantum cascade lasers at CUBRC[C], 1329(2007).

[58] Parker R A, Carr Z R, Dufrene A T et al. Space launch system base heating test: tunable diode laser absorption spectroscopy[C], 548(2016).

[59] Dufrene A T, MacLean M G, Carr Z R et al. Scaled rocket testing in hypersonic flow[C], 3550(2015).

[60] Parker R, MacLean M, Dufrene A et al. Emission measurements from high enthalpy flow on a cylinder in the LENS-XX hypervelocity expansion tunnel[C], 1058(2013).

[61] MacLean M G, Dufrene A T, Carr Z R et al. Measurements and analysis of Mars entry, decent, and landing aerothermodynamics at flight-duplicated enthalpies in LENS-XX expansion tunnel[C], 1897(2015).

[62] Finch P M, Girard J, Strand C et al. Measurements of time-resolved air freestream nitric oxide rotational, vibrational temperature and concentration in the T5 reflected shock tunnel[C], 3714(2020).

[63] Finch P M, Girard J J, Schwartz T et al. Measurements of T5 shock tunnel freestream temperature, velocity, and composition[J]. AIAA Journal, 61, 1555-1578(2023).

[64] Krishna Y, Sheehe S L, O’Byrne S B. A time-resolved temperature measurement system for free-piston shock tunnels[C], 2249(2015).

[65] O’Byrne S, Gai S L, Kaseman T et al. Thermal nonequilibrium in hypersonic separated flow[R](2014).

[66] Krishna Y, Sheehe S L, O’Byrne S. Detection of spatial variation in hypersonic nozzle flow using diode laser spectroscopy[J]. AIAA Journal, 56, 2930-2935(2018).

[67] Krishna Y, O’Byrne S, Aizengendler M, Bonazza R, Ranjan D. Diode-laser-based driver gas detector for hypersonic shock tunnels[M]. International symposium on shock waves, 611-616(2015).

[68] Krishna Y. Diode laser spectroscopy for high-enthalpy facility and hypersonic flight characterisation[EB/OL]. https://unsworks.unsw.edu.au/entities/publication/6c6d8457-949f-4ee5-9869-dca975525620/full

[69] Matsuda A, Fujita K, Sato S et al. Absorption spectroscopy for temperature measurement behind shock waves at super-orbital velocity[J]. Journal of Thermophysics and Heat Transfer, 19, 294-299(2005).

[70] Tanno H, Komuro T, Sato K et al. Laser absorption spectroscopy for determination of flow characteristics in high enthalpy shock tunnel[C], 8002(2006).

[71] Meyers J, Paris S, Fletcher D. Development of diode laser absorption instrument for free stream measurements in hypervelocity CO2 flows[C], 4138(2008).

[72] Meyers J M, Fletcher D. Diode laser absorption sensor design and qualification for CO2 hypersonic flows[J]. Journal of Thermophysics and Heat Transfer, 25, 193-200(2011).

[73] Meyers J, Paris S, Fletcher D. Diode laser absorption measurements of free stream hypervelocity CO2 flow at 1.6 µm[C], 4326(2009).

[74] Meyers J M, Paris S, Fletcher D G. Characterization of CO2 flow in a hypersonic impulse facility using DLAS[J]. Experiments in Fluids, 57, 25(2016).

[75] Dudas E, Anfuso E, Grossir G et al. Laser absorption spectroscopy of Rb for enhanced hypersonic wind tunnel flow characterization[C](2022).