Abstract
Single shot spatially and spectrally resolved laser induced predissociation fluorescence measurements in a shock layer around a cylinder in a pulsed supersonic free stream are presented. Fluoresence signals were produced using the tuned output of an argon fluoride excimer laser to excite a mixture of rovibrational transitions in molecular oxygen. The signals produced along a line inside the shock layer were focussed onto a two dimensional detector coupled to a spectrometer, thus allowing spectral and spatial resolution of the fluoresence. In this way, it was possible to detect two fluoresence signals from two different transitions simultaneously, allowing the determination of vibrational temperatures without the need for calibration. To minimize problems associated with low signal to noise ratios, background subtraction and spatial averaging was required.
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Andresen P, Bath A, Gröger W, Lülf HW, Meijer G, ter Meulen JJ (1988) Laser-induced fluorescence with tunable excimer lasers as a possible method for instantaneous temperature field measurements at high pressures: checks with an atmospheric flame. Applied Optics 27:365
Andresen P, Meijer G, Schulter H, Voges H, Koch A, Hentschel W, Oppermann W, Rothe E (1990) Fluorescence imaging inside an internal combustion engine using tunable excimer laser. Applied Optics 29:2392
Barlow RS, Colligan A (1991) Linear LIF measurements of OH in nonpremixed methane-air flames: when are quenching corrections unnecessary? AIAA 29th Aerospace Sciences Meeting, Reno, AIAA 91-0179
Berg JO, Shackleford WL (1979) Rotational redistribution effect on saturated laser-induced fluorescence. Applied Optics 18:2093
Campbell DH (1982) Vibrational level relaxation effects on laser-induced fluorescence measurements of hydroxide number density in a methaneair flame. Applied Optics 21:2912
Campbell DH (1984) Collisional effects on laser-induced fluorescence measurements of hydroxide concentrations in a combustion environment: effects forv′=0 excitation. Applied Optics 23:689
Carter CD, Salmon JT, King GB, Laurendeau (1987) Feasibility of hydroxyl concentration measurements by laser-saturated fluorescence in high-pressure flames. Applied Optics 26:4551
Chan C, Daily JW (1980a) Measurement of temperature in flames using laser induced fluorescence spectroscopy of OH. Applied Optics 19:1963
Chan C, Daily JW (1980b) Laser excitation dynamics of OH in flames. Applied Optics 19:1357
Creek DM, Nicholls RW (1975) A comprehensive re-analysis of the O2(B3 ∑ −u −X3 ∑ −g ) Schumann-Runge band system. Proc R Soc Lond A 341:517
Davies L (1967) The interaction of the reflected shock with the boundary layer in a shock tube and its influence on the duration of hot flow in the reflected-shock tunnel, part 1. Ministry of Aviation, London, CD No. 880
Dyer MJ, Crosley DR (1982) Two dimensional imaging of OH laserinduced fluorescence in a flame. Optic Letters 7:382
Ebrahim N, Sandeman RJ (1977) Spatially resolved excitation temperature measurements in a hypersonic flow using the hook method. Applied Optics 16:1376
Friedman RS (1990) J Quantum Spectrosc Radiat Transfer 43:225
Hanson HK (1987) Combustion diagnostics: planar flowfield imaging. Twenty-First International Symposium on Combustion, The Combustion Institute Pittsburgh PA, pp 1677–1691
Hanson HK, Seitzman JM, Paul PH (1990) Planar laser-fluorescence imaging of combustion gases. Applied Physics B 50:441
Harris R, Blackledge M, Generosa J (1969) Rydberg-Klein-Rees (RKR) Franck-Condon factors for the O2 Schumann-Runge system including high vibrational quantum numbers. J Molec Spectrosc 30:506
Herzberg G (1950) Molecular spectra and molecular structure: vol 1, spectra of diatomic molecules. Van Nostrand Reinhold, New York
Hiller B, Hanson RK (1988) Simultaneous planar measurements of velocity and pressure fields in gas flows using laser-induced fluorescence. Applied Optics 27:33
Hornung HG (1972) Non-equilibrium dissociating nitrogen flow over spheres and circular cylinders. J Fluid Mech 53:149
Kelly PB, Hudson RS (1985) Chem Phys Lett 114:45
Ketterle W, Schäfer M, Arnold A, Wolfrum J (1992) 2D single-shot imaging of OH radicals using tunable excimer lasers. Applied Physics B 54:109
Kim G-S, Hitchcock LM, Rothe EW, Reck GP (1991) Identification and imaging of hot O2(v′'=2, 3, or 4) in hydrogen flames using 193 nmand 210 nm-range light. Applied Physics B 53:180
Kychakoff G, Howe RD, Hanson RK (1984) Quantitative flow visualization technique for measurements in combustion gases. Applied Optics 23:704
Landau L, Teller E (1936) Zur Theorie der Schalldispersion. Physik Z Sowjetunion 10, 1:34
Lee MP, Paul PH, Hanson RK (1987) Quantitative imaging of temperature fields in air using planar laser-induced fluorescence of O2. Optics Letters 12:75
Lewis BR, Berzins L, Carver JH, Gibson ST (1986) Rotational variation of predissociation linewidth in the Schumann-Runge Bands of16O2. J Quant Spectrosc Radiat Transfer 36:187
Lucht RP, Laurendeau NM, Sweeney DW (1982) Temperature measurements by two-line laser-saturated OH fluorescence in flames. Applied Optics 21:3729
Lucht RP, Sweeney DW, Laurendeau NM (1980) Balanced cross-rate model for saturated molecular fluorescence in flames using a nanosecond pulse length laser. Applied Optics 19:3295
Palma PC, Houwing AFP, Sandeman RJ (1993) Absolute intensity measurements of impurity emissions in a shock tunnel and their consequences for laser induced fluorescence experiments. Shock Waves 3:49–53
Palmer JL, McMilin BK, Hanson RK (1992) Planar laser-induced fluorescence imaging of velocity and temperature in shock tunnel free jet flow. 30th Aerospace Sciences Meeting and Exhibit, Reno, NV
Palmer JL, McMillin BK, Lee MP, Hanson RK (1991) Two-dimensional imaging of shock tube flows using planar laser-induced fluorescence. In: Takayama K (ed) 18th International Symposium of Shock Waves, Sendai, Japan
Seitzman JM, Hanson RK (1992) Quantitative fluorescence imaging: a comparison of linear, predissociative and saturated pumping techniques. American Institute of Aeronautics and Astronautics, 30th Aerospace Sciences Meeting, Reno, NV, paper 92-0879
Smith CE (1966) The starting process in a hypersonic nozzle. J Fluid Mech 24:625
Stalker RJ (1967) A study of the free piston shock tunnel. AIAA J 5:2160
Stalker RJ, Crane KC (1977) Mass spectrometric analysis hypersonic flows. J Phys D 10:679
Stepowski D, Cottereau MJ (1981) Study of the collisional lifetime of hydroxyl (su2∑ +,v′=0) radicals in flames by time-resolved laser-induced fluorescence. Combust Flame 40:65
Tatum JB, Watson JKG (1971) Rotational line strengths in3 ∑ ± −3 ∑ ± transitions with intermediate coupling. Can J Phys 49:2693
Vardavas IM (1984) Modelling reactive gas flows within shock tunnels. Aust J Phys 37:157
Vincenti WG, Kruger CH (1986) In: Introduction to physical gas dynamics. John Wiley & Sons Inc, pp 204–205
Yang X, Wodtke AM (1991) Direct observation of orbit rotation predissociation in the O2 Schumann-Runge system. J Chem Phys 94:2469
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Sutton, D.J., Houwing, A.F.P., Palma, P.C. et al. Vibrational temperature measurements in a shock layer using laser induced predissociation fluorescence. Shock Waves 3, 141–148 (1993). https://doi.org/10.1007/BF02115893
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DOI: https://doi.org/10.1007/BF02115893