Potential for energy recovery from boundary-layer ingesting actuator disk propulsion

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dc.contributor.author Mutangara, Ngonidzashe E.
dc.contributor.author Smith, Lelanie
dc.contributor.author Craig, K.J. (Kenneth)
dc.contributor.author Sanders, Drewan S.
dc.date.accessioned 2024-03-27T12:42:02Z
dc.date.available 2024-03-27T12:42:02Z
dc.date.issued 2024
dc.description.abstract The theoretical benefits of highly integrated propulsion systems are highlighted herein by assessing the potential for energy recovery utilization using actuator disk propulsion. Decomposing aerodynamic forces into thrust and drag for closely integrated bodies, particularly those employing boundary-layer ingestion, becomes challenging. In this work, a mechanical energy-based approach was taken using the power balance method. This allowed the performance to be analyzed through the mechanical flow power in the fluid domain, disregarding the need for any explicit definition of thrust and drag. Through this, the benefit of boundary-layer ingestion was observed from a wake energy perspective as a decrease in the downstream mechanical energy deposition and associated viscous dissipation. From a propulsion perspective, the reduction in power demand necessary to produce propulsive force indicated the possibility of power savings by utilizing the energy contained within the ingested boundary-layer flow. en_US
dc.description.department Mechanical and Aeronautical Engineering en_US
dc.description.librarian hj2024 en_US
dc.description.sdg None en_US
dc.description.sponsorship The University of Pretoria Department of Research and Innovation as well as the Cranfield School of Aerospace, Transport, and Manufacturing. en_US
dc.description.uri https://arc.aiaa.org/toc/ja/0/0 en_US
dc.identifier.citation Mutangara, N.E., Smith, L., Craig, K.J. et al. 2024, 'Potential for energy recovery from boundary-layer ingesting actuator disk propulsion', Journal of Aircraft, doi : 10.2514/1.C037294. NYP. en_US
dc.identifier.issn 0021-8669 (print)
dc.identifier.issn 1533-3868 (online)
dc.identifier.other 10.2514/1.C037294
dc.identifier.uri http://hdl.handle.net/2263/95394
dc.language.iso en en_US
dc.publisher American Institute of Aeronautics and Astronautics en_US
dc.rights © 2024 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. en_US
dc.subject Energy recovery en_US
dc.subject No slip condition en_US
dc.subject Propulsive efficiency en_US
dc.subject Aerodynamic configurations en_US
dc.subject NACA 0012 en_US
dc.subject Boundary layer ingestion en_US
dc.subject Computational fluid dynamics (CFD) en_US
dc.subject Skin friction en_US
dc.title Potential for energy recovery from boundary-layer ingesting actuator disk propulsion en_US
dc.type Postprint Article en_US


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