Detonation limits in mixtures of oxygen and homologous hydrocarbons
Detonation parameters have been determined for fuel+ oxygen mixtures for ambient pressure and temperature in a 1 in (2.54 cm) diameter tube, with initiating impact from a detonating stochiometric hydrogen + oxygen mixture. Detonation limits in mole percent fuel are : methane 8.25 and 55.80 n -propane 2.50 and 42.50 n -butane 2.05 and 37.95 neopentane 1.50 and 33.00 propylene 2.50 and 50.00 These data have been matched with comparable results for the systems oxygen + ethane and oxygen + ethylene, obtained in other researches, in order to establish behaviour in homologous series of com pounds. For all compositions, propagation of detonation can usefully be correlated to the Mach product v M 2 . Far-reaching correlations are found for different hydrocarbon molecules, when the data are transformed on a homology basis. This suggests that the structure of the fuel molecules has only a secondary influence. At the fuel-lean limits, marginal behaviour can be interpreted in terms of a critical temperature rise which may be related to a critical rate of an initial cracking mechanism . Near the fuel-rich limits it seems more likely that stability depends on the condensation of (carbonaceous) solids from a mixture of cracking products.