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Aerodynamic-wave break-up of liquid sheets in swirling airflows and combustor modules
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ingebo, R. |
| Copyright Year | 1983 |
| Description | Experimental mean drop diameter data were obtained for the atomization of liquid sheets injected axially downstream in high velocity swirling and nonswirling airflow. Conventional simplex pressure atomizing fuel nozzles and splash type fuel injectors were studied under simulated combustor inlet airflow conditions. A general empirical expression relating recirprocal mean drop diameter to airstream mass velocity was obtained and is presented. The finest degree of atomization, i.e., the highest value of the coefficient C, was obtained with swirl can combustor modules (C = 15) as compared with pressure atomizing nozzles (C = 12). |
| File Size | 809296 |
| Page Count | 15 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830015274 |
| Archival Resource Key | ark:/13960/t53f9kr2v |
| Language | English |
| Publisher Date | 1983-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Air Flow Particle Size Distribution Inlet Nozzles Flow Velocity Fuel Injection Combustion Chambers Liquid Injection Atomizing Mass Flow Swirling Drops Liquids Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
