1958
DOI: 10.1021/ie50577a032
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Shock Tube Technique for Study of Autoignition of Liquid Fuel Sprays

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Cited by 12 publications
(6 citation statements)
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“…The shock tube, fuel injection system, and most of the experimental apparatus have been described previously (8,9).…”
Section: Methodsmentioning
confidence: 99%
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“…The shock tube, fuel injection system, and most of the experimental apparatus have been described previously (8,9).…”
Section: Methodsmentioning
confidence: 99%
“…A shock tube technique (8) was used to provide a source of stationary, high pressure-high temperature air. Several liquid fuels were sprayed into the zone of compressed air after reflection of the incident shock wave from the tube end.…”
mentioning
confidence: 99%
“…Perhaps the first example of an aerosol shock tube was a device engineered by Mullaney in 1958 for use with n-hexadecane droplets [37,38]. Mullaney's shock tube introduced fuel using a modified diesel injector system.…”
Section: Aerosol Loading In Shock Tubesmentioning
confidence: 99%
“…In contrast, shocks in aerosols require a fuel measurement after droplet evaporation is complete, because techniques of quantifying the amount of fuel aerosol in the Region 1 mixture (e.g., using Mie scattering [60]) are difficult. (Note that in shock tubes that employ aerosol injection systems [37,38], simply measuring the volume of liquid that is injected is possible; however, nonuniformity in the aerosol concentration throughout the shock tube and losses of aerosol to the tube walls make this technique less reliable.) This is best accomplished by way of a spectroscopic laser diagnostic using the Beer-Lambert relation.…”
Section: Quantifying Fuel Loadingmentioning
confidence: 99%
“…A study of the combustion process when re-hexadecane is injected as a fine spray into shock-heated air was made by Mullaney (5). By high-speed photography, he was able to observe injection of the spray, evaporation of the droplets, and spontaneous ignition.…”
mentioning
confidence: 99%