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• W3014299522 abstract "No AccessFull-Length PapersData and Design Models for Civil Turbopropeller AircraftBenoît G. Marinus and Lucile QuodbachBenoît G. MarinusRoyal Military Academy, 1000 Brussels, Belgium*Associate Professor, Department of Mechanical Engineering. Senior Member AIAA.Search for more papers by this author and Lucile QuodbachRoyal Military Academy, 1000 Brussels, Belgium†Department of Mechanical Engineering.Search for more papers by this authorPublished Online:2 Apr 2020https://doi.org/10.2514/1.C035271SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Ryerson M. and Hansen M., “The Potential of Turboprops for Reducing Aviation Fuel Consumption,” Transportation Research, Part D: Transport and Environment, Vol. 15, No. 6, 2010, pp. 305–314. https://doi.org/10.1016/j.trd.2010.03.003 CrossrefGoogle Scholar[2] Davendralingam N. and Crossley W., “Robust Approach for Concurrent Aircraft Design and Airline Network Design,” Journal of Aircraft, Vol. 51, No. 6, 2014, pp. 1773–1783. https://doi.org/10.2514/1.C032442 LinkGoogle Scholar[3] Roskam J., Airplane Design—Part 1: Preliminary Sizing of Airplanes, Airplane Design, DARcorporation, Lawrence, KS, 2002. 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Google Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byDesign and aerodynamic evaluation of a medium short takeoff and landing tactical transport aircraft3 June 2021 | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 236, No. 5Technical Advances in Aviation Electrification: Enhancing Strategic R&D Investment Analysis through Simulation Decomposition31 December 2021 | Sustainability, Vol. 14, No. 1 What's Popular Volume 57, Number 6November 2020 CrossmarkInformationCopyright © 2020 by B. G. Marinus. 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. TopicsAircraft Components and StructureAircraft Conceptual DesignAircraft DesignAircraft OperationsAircraft Operations and TechnologyAircraft Stability and ControlAircraft StabilizerAircraft Wing DesignAircraftsTakeoff and LandingWing ConfigurationsWing Planforms KeywordsPropeller AircraftMaximum Takeoff WeightAircraft ConfigurationsHigh Aspect RatioAerodynamic PropertiesUnswept WingsPower Specific Fuel ConsumptionWing GeometryMean Aerodynamic ChordFuel Mass FractionAcknowledgmentThe authors wish to acknowledge the scientific and technological research initiative of the Belgian Defense for its partial funding of the present study under grant MSP-16/07.PDF Received8 October 2018Accepted7 February 2020Published online2 April 2020" @default.
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