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Range Equation for Hybrid-Electric Aircraft with Constant Power Split

2020; American Institute of Aeronautics and Astronautics; Volume: 57; Issue: 3 Linguagem: Inglês

10.2514/1.c035734

1533-3868

Reynard de Vries, Maurice Hoogreef, Roelof Vos,

Advanced Battery Technologies Research

No AccessEngineering NotesRange Equation for Hybrid-Electric Aircraft with Constant Power SplitReynard de Vries, Maurice F. M. Hoogreef and Roelof VosReynard de VriesDelft University of Technology, 2629 HS Delft, The Netherlands*Ph.D. Candidate, Faculty of Aerospace Engineering; . Member AIAA.Search for more papers by this author, Maurice F. M. HoogreefDelft University of Technology, 2629 HS Delft, The Netherlands†Assistant Professor, Faculty of Aerospace Engineering; . Member AIAA.Search for more papers by this author and Roelof VosDelft University of Technology, 2629 HS Delft, The Netherlands‡Assistant Professor, Faculty of Aerospace Engineering; . Associate Fellow AIAA.Search for more papers by this authorPublished Online:27 Apr 2020https://doi.org/10.2514/1.C035734SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Anon., “Realising Europe’s Vision for Aviation: Strategic Research & Innovation Agenda, Vol. 1,” Advisory Council for Aviation Research and Innovation in Europe, 2012. Google Scholar[2] Bonet J. T., Schellenger H. G., Rawdon B. K., Elmer K. R., Wakayama S. R., Brown D. L. and Guo Y., “Environmentally Responsible Aviation (ERA) Project—N+2 Advanced Vehicle Concepts Study and Conceptual Design of Subscale Test Vehicle (STV): Final Report,” NASA CR-2011-216519, Dec. 2011. 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Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3868 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsAerospace SciencesAircraft Components and StructureAircraft DesignAircraft Operations and TechnologyAircraft Stability and ControlAircraft Weight MeasurementsAircraft Wing DesignAircraftsElectric AircraftFlight DynamicsFlight Mechanics KeywordsHybrid Electric AircraftBréguet Range EquationLift to Drag RatioEnergy DensityEnergy ConsumptionPower Management and DistributionOperating Empty WeightAircraft ConfigurationsFree Body DiagramAerodynamic EfficiencyAcknowledgmentsThis work was partially funded by the European Union Horizon 2020 program, as part of the Clean Sky 2 program, Large Passenger Aircraft (CS2-LPA-GAM-2018-2019-01).PDF Received23 September 2019Accepted20 March 2020Published online27 April 2020