No AccessDeveloping a Digital Thread / Digital Twin Aerodynamic Performance Authoritative Truth SourceEdward M. KraftEdward M. KraftUniversity of Tennessee, TullahomaSearch for more papers by this authorAIAA 2018-4003Session: Design Optimization and Model Based Design IPublished Online:24 Jun 2018https://doi.org/10.2514/6.2018-4003SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byOSLC Implementation for Authoritative Source of Truth Construction in Aircraft Design: A Comprehensive Case Study5 Jul 2024El Gemelo Digital y su aplicación en la Automática16 February 2024 | Revista Iberoamericana de Automática e Informática industrial, Vol. 21, No. 2Design and Modelling of Digital Twin Technology to Improve Freight Logistics14 June 2023The use of “digital twins” technology in the operation of buildings and structures9 August 2023 | E3S Web of Conferences, Vol. 410THE USE OF DIGITAL TWINS TECHNOLOGY IN THE OPERATION OF BUILDINGS AND STRUCTURES27 Jun 2022 | Construction and Architecture, Vol. 10, No. 2Applying Blockchain Technology on Model-Based Systems EngineeringKwok-Bun Yue, Mark Guerra, Howard Wagner, Joses Sandeep Thamarai Selvan, Kayaanoosh Collector, Victor Tang, Margo Sikes, Kewei Sha, Pavani Kallempudi, Sahar Mardani and Keshav Kasichainula4 January 2021 What's Popular 2018 Aviation Technology, Integration, and Operations Conference June 25-29, 2018Atlanta, Georgiahttps://doi.org/10.2514/6.2018-4003 CrossmarkInformationCopyright © 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. TopicsAerodynamic PerformanceAerodynamicsAeronauticsAerospace SciencesAircraft Components and StructureAircraft DesignAircraft OperationsAircraft Operations and TechnologyAircraft Wing DesignAircraftsAviationAviation SafetyFlight TestFlight TrainingWind Tunnels KeywordsAerodynamic PerformanceFlight VehicleAircraft ConfigurationsFlight TestingSurrogate ModelWind Tunnel TestsModel Based System EngineeringLift to Drag RatioAircraft OperationsProduct Lifecycle ManagementDigital Topics Aircraft Design and Integration