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- W3148575562 abstract "AERODYNAMIC-NAVE BREAK-UP OF LIQUID SHEETS IN SWIRLING AIRFLOWS AND COnBUSTOR WWLES R. Ingebo National Aeronautics and Space Administration Lewis Research Center Cleveland, Ohio Abstract Experimental mean drop diameter data were obtained for the atomization of liquid sheets injected axially downstream in high-velocity swirling and non-swirling airflow. Conventional simplex pressure-atomizing fuel nozzles and splash-type fuel injectors were studied under simulated cornbustor inlet airflow conditions. The following general empirical expressi n re- * lating reciprocal mean drop dii.meter," @default.
- W3148575562 created "2021-04-13" @default.
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- W3148575562 date "1983-01-01" @default.
- W3148575562 modified "2023-09-27" @default.
- W3148575562 title "Aerodynamic-Wave Break-up of Liquid Shezts is 3wirling Airflows and Co;.).bustor Modules" @default.
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