No AccessMultidisciplinary Design Optimization Analysis of Flexible Solar-Regenerative High-Altitude Long-Endurance AircraftTaylor G. McDonnell, Judd A. Mehr and Andrew NingTaylor G. McDonnellBrigham Young UniversitySearch for more papers by this author, Judd A. MehrBrigham Young UniversitySearch for more papers by this author and Andrew NingBrigham Young UniversitySearch for more papers by this authorAIAA 2018-0107Session: Aircraft Design Optimization IPublished Online:7 Jan 2018https://doi.org/10.2514/6.2018-0107SectionsPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesRelated articlesCorrection: Multidisciplinary Design Optimization Analysis of Flexible Solar-Regenerative High-Altitude Long-Endurance Aircraft26 Jan 2018AIAA SciTech Forum What's Popular 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 8–12 January 2018Kissimmee, Floridahttps://doi.org/10.2514/6.2018-0107 CrossmarkInformationCopyright © 2018 by Taylor McDonnell, Judd Mehr, and Andrew Ning. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAircraft Components and StructureAircraft DesignAircraft Design SoftwareAircraft Operations and TechnologyAircraft Stability and ControlAircraft Wing DesignAircraftsLongitudinal Static StabilityUnmanned Aerial VehicleWing ConfigurationsWing Planforms KeywordsTransport AircraftHigh Altitude Long EnduranceMultidisciplinary Design OptimizationCarbon Fiber Reinforced PolymersAircraft DesignAerodynamic PropertiesNonlinear AeroelasticityLongitudinal StabilityAerodynamic PerformanceAircraft Configurations Topics Multidisciplinary Design Optimization