Observations were made of the behavior of a fuel droplet suspended in air in the collision plane of oppositely facing shock waves of equal strengths. In such situation the gas surrounding the droplet is brought almost instantaneously to a high-temperature stagnation state, and the rapid atomization process observed in the incident-shock experiment does not take place. Three kinds of liquid fuels were used. The temperature of the stagnant region ranged from 1000 to 3000°K, strong emissions indicating exothermic reactions being observed except near the lower temperature limit. A fairly short but definite induction period for the onset of strong emission, exhibiting an Arrhenius-type dependence on temperature, was found to exist, during which the droplet remained seemingly unaffected. The breakup of the droplet set in only after the emission, whereby the whole liquid mass exploded symmetrically into minute fragments, luminous zones spreading out with them. While the present experiment might be regarded as the extension of quasistatic ignition studies in furnace to higher temperatures, the features disclosed seem to indicate that a substantial role is played by the strong turbulence behind the reflected shock waves, resulting in an abnormally rapid heating of the droplet.
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