Ultra-Short Nacelles for Low Fan Pressure Ratio Propulsors
As the propulsor fan pressure ratio (FPR) is decreased for improved fuel burn, reduced emissions and noise, the fan diameter grows and innovative nacelle concepts with short inlets are required to reduce their weight and drag. This paper addresses the uncharted inlet and nacelle design space for low...
| Main Authors: | , , , |
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| Other Authors: | |
| Format: | Article |
| Published: |
American Society of Mechanical Engineers
2018
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| Online Access: | http://hdl.handle.net/1721.1/116091 https://orcid.org/0000-0003-2167-9860 |