The spray characteristics of fuels when sprayed under superheated and elevated fuel pressure are markedly different than traditional fuel injection sprays. Studying fuel sprays under these conditions will help us understand the complex behaviors that may provide us with information to optimize future applications of certain technologies like supercritical spray combustion. In this work optical diagnostics are used to study the behavior of Jet A-1 under subcritical, transcritical, and supercritical sprays into open air test chambers. The experimental setup includes a high-pressure air driven pump to create the required high fuel pressure and a special heated injector to increase the temperature of the fuel inside the injector before injection to the required temperatures. Optical techniques like Schlieren and backlit shadowgraph are used to capture and study the sprays from a single hole high pressure diesel injector. A combination of 4 different temperatures and 4 different pressures are tested and the resultant images are processed to obtain quantitative measurements such as spray penetrations, spray cone angle, and spray optical density for each case. Moreover, the spray plume structure transition with changing parameters from subcritical, transcritical, and supercritical states for the fuel are also studied. The results show that with the fuel being in a transcritical state before injection there is a measurable variation in the spray cone formation and penetration for any fixed pressure. At this state the spray cone shows a bimodal spray angle distribution with increasing penetration. An increase in vapor turbulence is also observed indicating the occurrence of flash boiling of the fuel. With the fuels pushed to a supercritical state, the spray shows a thinner spray jet near the injector with a reduced overall penetration and reduced optical density near nozzle. The transition between the three different states as shown in this study gives us an interesting relationship between the spray penetration, spray cone angle and the spray optical density. This can be used as an indicator in understanding spray atomization of the fuels under supercritical spray conditions.
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This content will become publicly available on May 14, 2024
Experimental Spray Characterization for Jet-A1 Under Temperature Controlled Subcritical, Transcritical, and Supercritical Spray Conditions
Fuels when sprayed under superheated and elevated fuel pressure show different behavior than traditional fuel injection sprays. In this work optical diagnostics were used to study the behavior of Jet A-1 under subcritical, transcritical, and supercritical sprays into open air ambience. Five different temperatures were tested, and the resultant spray images were processed to obtain quantitative measurements such as spray penetrations, and spray cone angle for each case. The spray structure transition with changing parameters from subcritical, transcritical, and supercritical states were also studied. The transition between the three different states are shown in this study and the resulting spray cone angles and penetrations are compared for the fuel. The results show that a transcritical spray has a measurable variation in the spray cone formation and penetration process for a fixed injection pressure. At this state the spray cone shows a bimodal spray angle relationship with increasing penetration. Flash boiling of the fuel is observed near the nozzle of the injector. Increasing the temperature further into the supercritical regime, the spray plume shows a thinning of the jet near the nozzle with a reduced overall penetration compared to lower temperatures.
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- Award ID(s):
- 2104394
- NSF-PAR ID:
- 10426838
- Date Published:
- Journal Name:
- Proceedings of 14th Asia-Pacific Conference on Combustion
- Format(s):
- Medium: X
- Sponsoring Org:
- National Science Foundation
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