A sizing and vehicle matching methodology for boundary layer ingesting propulsion systems
Boundary layer ingesting (BLI) propulsion systems offer potential fuel burn reduction for civil aviation and synergize with new advanced airframe concepts. However, the distorted inlet flow for BLI systems can cause performance and stability margin loss. System level analyses generally size a singl...
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| Format: | Others |
| Language: | en_US |
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Georgia Institute of Technology
2016
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| Online Access: | http://hdl.handle.net/1853/54408 |