NASA NTRS · 19830003976
Antimisting kerosene atomization and flammability
Abstract
Various parameters found to affect the flammability of antimisting kerosene (Jet A + polymer additive) are investigated. Digital image processing was integrated into a technique for measurement of fuel spray characteristics. This technique was developed to avoid many of the error sources inherent to other spray assessment techniques and was applied to the study of engine fuel nozzle atomization performance with Jet A and antimisting fuel. Aircraft accident fuel spill and ignition dynamics were modeled in a steady state simulator allowing flammability to be measured as a function of airspeed, fuel flow rate, fuel jet Reynolds number and polymer concentration. The digital imaging technique was employed to measure spray characteristics in this simulation and these results were related to flammability test results. Scaling relationships were investigated through correlation of experimental results with characteristic dimensions spanning more than two orders of magnitude.
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Fleeter, R., Petersen, R. A., Toaz, R. D., Jakub, A., Sarohia, V.. 1982-07-01. Antimisting kerosene atomization and flammability. https://ntrs.nasa.gov/citations/19830003976
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