The thermodynamic state of the hot gas behind reflected shock waves: Implication to chemical kinetics†

Procedures are discussed to correct for nonideality in a shock tube used in the reflected mode in conjunction with flash photolysis and atomic resonance absorption to measure chemical kinetics of atoms at high temperatures. Experimentally, pressure time profiles for the incident and reflectedshock regions are made close to the location of the observation windows through which absorbance is measured. The corresponding temperatures are calculated from the adiabatic equation of state. Justification for this procedure is provided by extending Mirels' boundary layer theory to take intoaccount interaction of the reflected wave with the flowing gas in the free stream and in the boundary layer. These theoretical methods are described for calculating the thermodynamic and hydrodynamic states behind the reflected wave from initial values of pressure and temperature and the measured velocity of the incident wave. The implication of these results to kinetic measurements at high temperature is discussed.

[1]  J. Sutherland,et al.  The flash photolysis—shock tube technique using atomic resonance absorption for kinetic studies at high temperatures , 1985 .

[2]  P. Frank,et al.  High temperature reaction rate for H+O2=OH+O and OH+H2=H2O+H , 1985 .

[3]  R. I. Soloukhin,et al.  Dynamics of flames and reactive systems. Proceedings of the Ninth International Colloquium on Gasdynamics of Explosions and Reactive Systems, Poitiers, France, July 3-8, 1983 , 1984 .

[4]  G. B. Skinner,et al.  Consistency of theory and experiment in the ethane–methyl radical system , 1981 .

[5]  H. Ando,et al.  Evaluation of boundary‐layer effects in shock‐tube studies of chemical kinetics , 1979 .

[6]  J. Troe Theory of thermal unimolecular reactions at low pressures. II. Strong collision rate constants. Applications , 1977 .

[7]  G. B. Skinner,et al.  Shock tube experiments on the pyrolysis of deuterium-substituted ethylenes , 1971 .

[8]  R. Hanson,et al.  Reflection of a shock wave into a density gradient , 1970 .

[9]  R. Strehlow,et al.  Shock Tube Technique in Chemical Kinetics , 1969 .

[10]  Harold Mirels,et al.  Flow Nonuniformity in Shock Tubes Operating at Maximum Test Times , 1966 .

[11]  H. B. Dyner Density Variation due to Reflected Shock‐Boundary‐Layer Interaction , 1966 .

[12]  S. Tsuchiya,et al.  Temperature Measurement of Argon Gas behind Reflected Shock Wave , 1965 .

[13]  H. Mirels Shock Tube Test Time Limitation Due to Turbulent-Wall Boundary Layer , 1964 .

[14]  Harold Mirels,et al.  TEST TIME IN LOW PRESSURE SHOCK TUBES , 1963 .

[15]  J. N. Bradley,et al.  Shock waves in chemistry and physics , 1963 .

[16]  J. C. Baird,et al.  Electron Paramagnetic Resonance Spectra of Some Disubstituted Nitric Oxides , 1961 .

[17]  G. Rudinger EFFECT OF BOUNDARY-LAYER GROWTH IN A SHOCK TUBE ON SHOCK REFLECTION FROM A CLOSED END , 1961 .

[18]  W. Gardiner,et al.  Density Measurements in Reflected Shock Waves , 1961 .

[19]  F. E. Belles,et al.  Limitations of the Reflected‐Shock Technique for Studying Fast Chemical Reactions , 1960 .

[20]  R. Strehlow,et al.  Limitations of the Reflected Shock Technique for Studying Fast Chemical Reactions , 1961 .

[21]  G. B. Skinner Limitations of the Reflected Shock Technique for Studying Fast Chemical Reactions , 1959 .

[22]  Russell E. Duff,et al.  Shock‐Tube Performance at Low Initial Pressure , 1959 .