High Pressure Single Pulse Shock Tube

1. High Pressure Single Pulse Shock Tube Kenneth Brezinsky, Mechanical and Industrial Engineering Sponsors: Department of Energy, National Science Foundation, National Aeronautical Space Administration, Office of Naval Research • Oxidation of Aromatic Compounds • Soot Formation Chemistry • High Pressure Carbon Monoxide Combustion • Rocket Nozzle Erosion Chemistry • High Pressure Shock Tube, Operating Range: • 5 atm < Pressure < 1000 atm • 800 K < Temperature < 3000 K • 0.5 ms < time < 2.0 ms • “Shock Tube Study of Thermal Rearrangement of 1,5-Hexadiyne over Wide Temperature and Pressure Regime”, J. Phys. Chem. A 2004, 108, 3406-3415 • “A High Pressure Model for the Oxidation of Toluene”, In Press, Proc. Int. Comb. Symp. 30, 2004 • “High Pressure, High Temperature Oxidation of Toluene”, Combustion and Flame, 139(4), 340-350, 2004 • “Ethane Oxidation and Pyrolysis from 5 bar to 1000 bar: Experiments and Simulation”.,In Press, International Journal of Chemical Kinetics, 2004 • “Chemical Kinetic Simulations behind Reflected Shock Waves”, Submitted, Int. J. Chem. Kin., 2005 • “Isomeric Product Distributions from the Self Reaction of Propargyl Radicals”, Submitted, J. Phys. Chem. 2005