Abstract
The feasibility of applying laser induced predissociation fluorescence (LIPF) to the measurement of vibrational temperatures in a shock layer flow around a cylinder in a pulsed supersonic free stream is examined. Single shot spatially and spectrally resolved LIPF measurements are presented and a comparison with theoretical predictions is made.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
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
Hanson RK, 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
Hiller B, and Hanson RK (1988) Simultaneous planar measurements of velocity and pressure fields in gas flows using laser-induced fluorescence. Applied Optics 27: 33
Kelly PB, Hudson RS (1985) Resonance fluorescence and resonance Raman spectra of molecular oxygen. Chem. Phys. Lett. 114: 45
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 nm- and 210 nm-range light. Applied Physics B 53: 180
Lewis BR, Berzins L, Carver JH, Gibson ST (1986) Rotational variation of predissociation linewidth in the Schumann-Runge Bands of 16O2- J. Quant. Spectrosc. Radiat. Transfer 36: 187
Mundt Ch (1992) Calculation of hypersonic, viscous non-equilibrium flows around reenrty bodies usinf a coupled boundary layer/Euler method. AIAA Paper 92–2856
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
Rein M (1989) Surf: A program for calculating inviscid supersonic reacting flows in nozzles. GALCIT FM 89–1
Seitzman JM, Hanson RK (1992) Quantitative fluorescence imaging: A comparison of linear, predissociative and saturated pumping techniques. AIAA 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
Sutton DJ, Houwing AFP, Palma PC, Sandeman RJ (1993) Vibrational temperature measurements in a shock layer using laer induced predissociation fluorescence. Shock Waves 3: 141
Tatum JB, Watson JKG (1971) Rotational line strengths in 3Σ± →3Σ± transitions with intermediate coupling. Can. J. Phys. 49: 2693
Vardavas IM (1984) Modelling reactive gas flows within shock tunnels. Austr. J. Phys. 37: 157
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 1995 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Sutton, D.J., Houwing, A.F.P., Palma, P.C., Sandeman, R.J. (1995). Vibrational Temperature Measurements in a Shock Layer Using Laser Induced Predissociation Fluorescence. In: Brun, R., Dumitrescu, L.Z. (eds) Shock Waves @ Marseille II. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-78832-1_4
Download citation
DOI: https://doi.org/10.1007/978-3-642-78832-1_4
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-78834-5
Online ISBN: 978-3-642-78832-1
eBook Packages: Springer Book Archive