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

dc.contributor.authorMutangara, Ngonidzashe E.
dc.contributor.authorSmith, Lelanie
dc.contributor.authorCraig, K.J. (Kenneth)
dc.contributor.authorSanders, Drewan S.
dc.date.accessioned2024-03-27T12:42:02Z
dc.date.available2024-03-27T12:42:02Z
dc.date.issued2024-03
dc.description.abstractThe 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.departmentMechanical and Aeronautical Engineeringen_US
dc.description.librarianhj2024en_US
dc.description.sdgNoneen_US
dc.description.sponsorshipThe University of Pretoria Department of Research and Innovation as well as the Cranfield School of Aerospace, Transport, and Manufacturing.en_US
dc.description.urihttps://arc.aiaa.org/toc/ja/0/0en_US
dc.identifier.citationMutangara, N.E., Smith, L., Craig, K.J. et al. 2024, 'Potential for energy recovery from boundary-layer ingesting actuator disk propulsion', Journal of Aircraft, vol. 6, no. 2, doi : 10.2514/1.C037294.en_US
dc.identifier.issn0021-8669 (print)
dc.identifier.issn1533-3868 (online)
dc.identifier.other10.2514/1.C037294
dc.identifier.urihttp://hdl.handle.net/2263/95394
dc.language.isoenen_US
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.rights© 2024 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.en_US
dc.subjectEnergy recoveryen_US
dc.subjectNo slip conditionen_US
dc.subjectPropulsive efficiencyen_US
dc.subjectAerodynamic configurationsen_US
dc.subjectNACA 0012en_US
dc.subjectBoundary layer ingestionen_US
dc.subjectComputational fluid dynamics (CFD)en_US
dc.subjectSkin frictionen_US
dc.titlePotential for energy recovery from boundary-layer ingesting actuator disk propulsionen_US
dc.typePostprint Articleen_US

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