Many experiments have been performed by various authors to measure the “thickness” of the reaction zone of gaseous detonations, i.e., the extension of the region where the main part of the chemical reaction takes place. These experiments have shown that at an initial pressure of 1 atmos the zone was too narrow to be resolved. Only in spinning detonations using modes close to the fundamental can one obtain a measure of the reaction time. Both spin and the dependence of the detonation velocity on the flow of the burned gas seem to be closely related to the mechanism of stabilization of a detonation. If the reaction rate is increased, rather high modes of fundamental spin frequency can be detected, which seem to disappear in very long tubes. This indicates a rather strong coupling between the burned gas and the reaction zone, the source of energy. The energy involved in the spin vibrations was found to decrease with increasing mode (frequency roughly proportional to n −1 ). The dependence of the detonation velocity on the flow conditions in the burned gas, also obtained experimentally, points at the coupling between reaction zone and flow in the burned gas. The end of the zone, in which the energy release which propagates the detonation takes place, lies in a region where chemical reaction is not yet finished. Using the conditions for flow through Mach-number 1, while taking into consideration heat addition, change of the effective tube area by boundary layer and the influence of expansion waves from the wall etc., and applying it to the velocity deficit of the real detonation, one can get an estimate of the state of chemical reaction at the area where M =1. This area seems to be rather sensitive to disturbances. In order to investigate the chemical reaction in the main part of the reaction zone, low pressure detonations were used. In overdriven detonations, where the stabilization effects mentioned above are rather unimportant, the reaction zone was fairly smooth. The conditions of normal detonations had to be chosen very carefully in order to obtain regular signals. In some hydrocarbon-O 2 systems, density gradients were determined. In the system H 2 −O 2 −N 2 density gradients, temperatures, OH-concentrations etc. were measured. The temperatures at the “end of the reaction” zone agreed with calculated temperatures within the limits of experimental error. Density, temperature and OH-concentration distribution correspond in principle to the model of Doering, von Neumann and Zeldovich. The chemical reaction, immediately following the shock front in H 2 −O 2 −N 2 mixtures could be described using the known kinetic data of the H 2 −O 2 reaction.
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