High Pressure Ignition of Boron in Reduced Oxygen Atmospheres
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AbstractBoron ignition delay times for 24 μm diameter particles have been measured behind the reflected shock at a shock tube endwall in reduced oxygen atmospheres and in a combustion bomb at higher pressures in the products of a hydrogen/oxygen/nitrogen reaction. The shock tube study independently varies temperature (1400 – 3200 K), pressure (8.5, 34 atm), and ignition-enhancer additives (water vapor, fluorine compounds). A combustion chamber is used at a peak pressure of 157 atm and temperature in excess of 2800 K to study ignition delays at higher pressures than are possible in the shock tube.
2012 ◽
Vol 184
(10-11)
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pp. 1635-1650
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2018 ◽
Vol 196
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pp. 478-486
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2015 ◽
Vol 35
(1)
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pp. 259-266
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