Chinese Journal of Lasers, Volume. 48, Issue 4, 0401005(2021)
Research Progress of Laser-Induced Fluorescence Technology in Combustion Diagnostics
[3] Sun M B, Wang H B, Cai Z et al. Unsteady supersonic combustion[M]. Singapore: Springer Singapore(2020).
[18] Ehn A, Zhu J J, Li X S et al. Advanced laser-based techniques for gas-phase diagnostics in combustion and aerospace engineering[J]. Applied Spectroscopy, 71, 341-366(2017).
[33] Chen S, Kapsta L, Weng W B et al. Simultaneous multi-species PLIF diagnostic on CH4-air inverse diffusion jet flame[J]. Journal of Experiments in Fluid Mechanics, 32, 26-32(2018).
[37] Medwell P R, Chan Q N. Kalt P A M, et al. Development of temperature imaging using two-line atomic fluorescence[J]. Applied Optics, 48, 1237-1248(2009).
[44] Halls B R, Gord J R, Hsu P S et al. Development of two-color 3D tomographic VLIF measurements. [C]∥2018 AIAA Aerospace Sciences Meeting, January 8-12, 2018, Kissimmee, Florida. Reston, Virginia: AIAA(2018).
[45] Chterev I, Rock N, Ek H et al. Simultaneous high speed (5 kHz) fuel-PLIE, OH-PLIF and stereo PIV imaging of pressurized swirl-stabilized flames using liquid fuels. [C]∥55th AIAA Aerospace Sciences Meeting, January 9-13, 2017, Grapevine, Texas. Reston, Virginia: AIAA(2017).
[46] Fugger C A, Yi T, Sykes J et al. The structure and dynamics of a bluff-body stabilized premixed reacting flow. [C]∥2018 AIAA Aerospace Sciences Meeting, January 8-12, 2018, Kissimmee, Florida. Reston, Virginia: AIAA(2018).
[47] Eckbreth A C. Laser diagnostics for combustion temperature and species[M]. ∥Culick F, Heitor M V, Whitelaw J H, et al. Unsteady Combustion. NATO ASI Series (Series E: Applied Sciences). Dordrecht: Springer, 306, 393-410(1996).
[48] Borggren J. Two-line atomic fluorescence for thermometry in reactive flows Lund,[D]. Sweden: Lund University(2018).
[53] Carter C D, Hammack S D, Lee T. High-speed planar laser-induced fluorescence of the CH radical using the C2Σ +-X2Π(0,0) band[J]. Applied Physics B Photophysics and Laser Chemistry, 116, 515-519(2014).
[60] Frank J H, Chen X L, Patterson B D et al. Comparison of nanosecond and picosecond excitation for two-photon laser-induced fluorescence imaging of atomic oxygen in flames[J]. Applied Optics, 43, 2588-2597(2004).
[66] Wang H B, Wang Z G, Sun M B et al. Combustion characteristics in a supersonic combustor with hydrogen injection upstream of cavity flameholder[J]. Proceedings of the Combustion Institute, 34, 2073-2082(2013).
[68] Cantu L M L, Gallo E C A, Cutler A D et al. OH PLIF visualization of a premixed ethylene-fueled dual-mode scramjet combustor. [C]∥54th AIAA Aerospace Sciences Meeting, January 4-8, 2016, San Diego, California, USA. Reston, Virginia: AIAA(2016).
[69] Geipel C M, Rockwell R D, Chelliah H K et al. High-spatial-resolution OH PLIF visualization in a cavity-stabilized ethylene-air turbulent flame. [C]∥33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, June 5-9, 2017, Denver, Colorado, USA. Reston, Virginia: AIAA(2017).
[70] Geipel C M, Cutler A D, Rockwell R D et al. Characterization of flame front structure in a dual-mode scramjet combustor with OH-PLIF. [C]∥AIAA Scitech 2019 Forum, January 7-11, 2019, San Diego, California. Reston, Virginia: AIAA(2019).
[72] Tian Y, Zeng X J, Yang S H et al[J]. injector position on flow structure, flame development in the scramjet combustor. Aerospace Science, Technology, 82/83, 9-19(2018).
[75] Micka D, Driscoll J. Reaction zone imaging in a dual-mode scramjet combustor using CH-PLIF. [C]∥44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 21-23, 2008, Hartford, CT. Reston, Virginia: AIAA(2008).
[77] Liang J H, Li Y, Sun M B et al. CH-PLIF imaging of flame heat-release structures in supersonic combustion[J]. Journal of National University of Defense Technology, 41, 27-33(2019).
[79] Allison P, Frederickson K, Kirik J W et al. Investigation of flame structure and combustion dynamics using CH2O PLIF and high-speed CH * chemiluminescence in a premixed dual-mode scramjet combustor. [C]∥54th AIAA Aerospace Sciences Meeting, January 4-8, 2016, San Diego, California, USA. Reston, Virginia: AIAA(2016).
[80] Gabet K N, Sutton J A. Narrowband versus broadband excitation for CH2O PLIF imaging in flames using a frequency-tripled Nd∶YAG laser[J]. Experiments in Fluids, 55, 1-11(2014).
[88] Liu J, Gen H, Zhai Z et al. Experimental investigation of transverse Jet in supersonic crossflow by acetone planar laser induced fluorescence. C]∥1st Modern Aerodynamics & Aerothermodynamics Conference: Proceedings of 1st Modern Aerodynamics & Aerothermodynamics Conference. Shanghai: Chinese Society of Aerodynamics, 582-587(2006).
[89] Zhou M. Research on measurements of air mixing ratio using acetone planar laser induced fluorescence[D]. Harbin: Harbin Institute of Technology(2015).
[96] Lozano A, Yip B, Hanson R K. Acetone: a tracer for concentration measurements in gaseous flows by planar laser-induced fluorescence[J]. Experiments in Fluids, 13, 369-376(1992).
[100] Miller V, Gamba M, Mungal G et al. Toluene PLIF thermometry in supersonic flows. [C]∥42nd AIAA Fluid Dynamics Conference and Exhibit, June 25-28, 2012, New Orleans, Louisiana. Reston, Virginia: AIAA(2012).
[105] Kashitani M, Yamaguchi Y, Handa T et al. Study on laser-induced acetone fluorescence in low-temperature gases of nitrogen and air. [C]∥50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, January 9-12, 2012, Nashville, Tennessee. Reston, Virginia: AIAA(2012).
[110] Cantu L M L. Visualization and analysis of a hydrocarbon premixed flame a in small scale scramjet combustor[D]. Washington: The George Washington University(2016).
[111] Chun J. Experimental investigations of injection, mixing, and reaction processes in supersonic flow applications Stuttgart,[D]. Gemany: University of Stuttgart(2009).
[114] Ji Y B, Yuan Y W, Ge B et al. 31(1): 48-[J]. dilution characteristics of a RQL, rich-quench-lean, combustor in its quenching zone in an aeroengine. Journal of Engineering for Thermal Energy, Power, 53, 131-132(2016).
[115] Yu Y. Experimental study and numerical simulation of gas flameless combustion induced by the inner structure[D]. Hefei: University of Science and Technology of China(2010).
[116] Dec J E, Canaan R E[2020-06-15]. PLIF imaging of NO formation in a DI diesel engine [2020-06-15].https:∥www.researchgate.net/publication/300690588_PLIF_Imaging_of_NO_Formation_in_a_DI_Diesel_Engine..
[122] Zhao W. Visualization research on gas injection characteristics of engine based on PLIF[D]. Harbin: Harbin Engineering University(2018).
[127] Snyder J A. Development and application of tracer-based planar laser-induced fluorescence imaging diagnostics for HCCI engines Stanford, California,[D]. USA: Stanford University(2011).
[135] Joklik R G, Daily J W. Two-line atomic fluorescence temperature measurement in flames:an experimental study[J]. Applied Optics, 21, 4158-4162(1982).
[138] Chan Q N, Medwell P R. Kalt P A M, et al. Simultaneous imaging of temperature and soot volume fraction[J]. Proceedings of the Combustion Institute, 33, 791-798(2011).
[140] Münsterjohann B. Huber F J T, Klima T C, et al. Potential of two-line atomic fluorescence for temperature imaging in turbulent indium-oxide-producing flames[J]. Journal of Nanoparticle Research, 17, 1-10(2015).
[144] Löfström C, Engström J, Richter M et al. Feasibility studies and application of laser /optical diagnostics for characterisation of a practical low-emission gas turbine combustor. [C]∥Proceedings of ASME Turbo Expo 2000: Power for Land, Sea, and Air, May 8-11, 2000, Munich, Germany. New York: ASME, 1-8(2000).
[148] Manteghi A A. Probing gases and flames by coherent rayleigh brillouin scattering and two lines atomic fluorescence Eindhoven,[D]. Netherlands: Eindhoven University of Technology(2013).
[153] Sijtsema N M, Dam N J. Klein-Douwel R J H, et al. Air photolysis and recombination tracking: a new molecular tagging velocimetry scheme[J]. AIAA Journal, 40, 1061-1064(2002).
[154] Bearden W C, Hall C A, Pitz R W. Examination of NO tag formation for unseeded molecular tagging velocimetry. [C]∥55th AIAA Aerospace Sciences Meeting, January 9-13, 2017, Grapevine, Texas. Reston, Virginia: AIAA(2017).
[155] ElBaz A M, Pitz R W. N2O molecular tagging velocimetry[J]. Applied Physics B, 106, 961-969(2012).
[157] Bathel B, Danehy P, Jones S et al. Trip-induced transition measurements in a hypersonic boundary layer using molecular tagging velocimetry. [C]∥51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, January 7-10, 2013, Grapevine (Dallas/Ft. Worth Region), Texas. Reston, Virginia: AIAA(2013).
[161] Ribarov L A, Hu S T, Wehrmeyer J A et al. Hydroxyl tagging velocimetry method optimization: signal intensity and spectroscopy[J]. Applied Optics, 44, 6616-6626(2005).
[163] Dam N. Klein-Douwel R J, Sijtsema N M, et al. Nitric oxide flow tagging in unseeded air[J]. Optics Letters, 26, 36-38(2001).
[165] Bathel B, Johansen C, Danehy P et al. Hypersonic boundary layer transition measurements using N O2->NO photo-dissociation tagging velocimetry. [C]∥41st AIAA Fluid Dynamics Conference and Exhibit, June 27-30, 2011, Honolulu, Hawaii. Reston, Virginia: AIAA(2011).
[166] Bathel B, Danehy P, Johansen C et al. Hypersonic boundary layer measurements with variable blowing rates using molecular tagging velocimetry. [C]∥28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference, June 25-28, 2012, New Orleans, Louisiana Reston, Virginia: AIAA(2012).
[167] Kidd F G, Narayanaswamy V, Danehy P M et al. Characterization of the NASA langley arc heated scramjet test facility using NO PLIF. [C]∥30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, June 16-20, 2014, Atlanta, GA. Reston, Virginia: AIAA(2014).
[171] Parziale N J, Smith M, Marineau E C. Krypton tagging velocimetry for use in high-speed ground-test facilities. [C]∥53rd AIAA Aerospace Sciences Meeting, January 5-9, 2015, Kissimmee, Florida. Reston, Virginia: AIAA(2015).
[174] Mustafa M A, Parziale N J, Marineau E C et al. Two-dimensional krypton tagging velocimetry (KTV-2D) investigation of shock-wave/turbulent boundary-layer interaction. [C]∥2018 AIAA Aerospace Sciences Meeting,January 8-12, 2018, Kissimmee, Florida. Reston, Virginia: AIAA(2018).
[176] Mustafa M A, Shekhtman D, Parziale N J. Single-laser krypton tagging velocimetry (KTV) investigation of air and N2 boundary-layer flows over a hollow cylinder in the stevens shock tube. [C]∥AIAA Scitech 2019 Forum, January 7-11, 2019, San Diego, California. Reston, Virginia: AIAA(2019).
[182] Pitz R, Lahr M, Douglas Z et al. Hydroxyl tagging velocimetry in a Mach 2 flow with a wall cavity. [C]∥43rd AIAA Aerospace Sciences Meeting and Exhibit, January 10-13, 2005, Reno, Nevada. Reston, Virginia: AIAA(2005).
[187] Hu Z Y, Ye J F, Zhang Z R et al. Development of laser combustion diagnostic techniques for ground aero-engine testing[J]. Journal of Experiments in Fluid Mechanics, 32, 33-42(2018).
[188] Pan F, Sánchez-González R. McIlvoy M H, et al. Simultaneous three-dimensional velocimetry and thermometry in gaseous flows using the stereoscopic vibrationally excited nitric oxide monitoring technique[J]. Optics Letters, 41, 1376-1379(2016).
[196] Halls B R, Hsu P S, Ethan L et al. 3D OH LIF measurements in a lifted flame. [C]∥55th AIAA Aerospace Sciences Meeting, January 9-13, 2017, Grapevine, Texas. Reston, Virginia: AIAA(2017).
[197] Liu N, Ma L. 3D flame measurements using tomography reconstruction integrating view registration. [C]∥AIAA Scitech 2020 Forum, January 6-10, 2020, Orlando, FL, USA. Reston, Virginia: AIAA(2020).
[207] Mitsingas C M, Hammack S D, Mayhew E K et al. Simultaneous high speed PIV and CH PLIF using R-branch excitation in the C2Σ +-X2Π (0, 0) band[J]. Proceedings of the Combustion Institute, 37, 1479-1487(2019).
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Jiajian Zhu, Minggang Wan, Ge Wu, Bo Yan, Yifu Tian, Rong Feng, Mingbo Sun. Research Progress of Laser-Induced Fluorescence Technology in Combustion Diagnostics[J]. Chinese Journal of Lasers, 2021, 48(4): 0401005
Special Issue: SPECIAL ISSUE FOR "NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY"
Received: Jul. 1, 2020
Accepted: Sep. 15, 2020
Published Online: Feb. 4, 2021
The Author Email: Zhu Jiajian (jjzhu@nudt.edu.cn)