Drag Management in High Bypass Turbofan Nozzles for Quiet Approach Applications

The feasibility of a drag management device that reduces engine thrust on approach by generating a swirling outflow from the fan (bypass) nozzle is assessed. Deployment of such "engine air-brakes" (EABs) can assist in achieving slower and/or steeper and/or aeroacoustically cleaner approach...

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Bibliographic Details
Main Authors: Shah, P., Robinson, A., Price, A.
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Format: Article
Published: ASME International 2018
Online Access:http://hdl.handle.net/1721.1/115052
https://orcid.org/0000-0003-2167-9860