No AccessApproach to Modeling Boundary Layer Ingestion using a Fully Coupled Propulsion-RANS ModelJustin S. Gray, Charles A. Mader, Gaetan K. Kenway and Joaquim R. R. A. MartinsJustin S. GrayNASA Glenn Research CenterSearch for more papers by this author, Charles A. MaderUniversity of Michigan, Ann ArborSearch for more papers by this author, Gaetan K. KenwayUniversity of Michigan, Ann ArborSearch for more papers by this author and Joaquim R. R. A. MartinsUniversity of Michigan, Ann ArborSearch for more papers by this authorAIAA 2017-1753Session: Aircraft Design Optimization IIIPublished Online:5 Jan 2017https://doi.org/10.2514/6.2017-1753SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byHybrid Electric Propulsion Design and Analysis Based on Regional Aircraft Mission3 April 2025 | World Electric Vehicle Journal, Vol. 16, No. 4Parameter Sensitivity Study on Inflow Distortion of Boundary Layer Ingested Turbofans4 August 2022 | Aerospace, Vol. 9, No. 8Aerodynamic Shape Optimization of a Transonic, Propulsion-Airframe-Integrated Airfoil SystemMatthew G. Lauer and Phillip J. Ansell20 June 2022Recent Advances in Boundary Layer Ingestion Technology of Evolving Powertrain Systems2 February 2022 | Sustainability, Vol. 14, No. 3Evaluation of a Regional Aircraft with Boundary Layer Ingestion and Electric-Fan PropulsorMaicon Secchi, Pedro Teixeira Lacava, Luis Gustavo Trapp and Raphael Felipe Gama Ribeiro20 July 2021 | Journal of Aircraft, Vol. 58, No. 6USM3D Analyses of Transonic Boundary Layer Thickener Configurations Applied to FuselageMichael D. Bozeman Jr., Alaa Elmiligui, Gregory S. Jones and William Milholen29 March 2021 | Journal of Aircraft, Vol. 58, No. 4A reduced order model for boundary layer ingestion map prediction at fan inlet of rear-mounted engine nacelleDavide Cinquegrana and Pier Luigi Vitagliano4 January 2021Performance bookkeeping for aircraft configurations with fuselage wake-filling propulsion integration2 December 2019 | CEAS Aeronautical Journal, Vol. 11, No. 2USM3D Analyses in Support of the NASA Langley 0.3-Meter Transonic Cryogenic Tunnel Test of Boundary-Layer Thickener ConfigurationsMichael D. Bozeman, Alaa A. Elmiligui, Gregory S. Jones and William E. Milholen5 January 2020Modeling hybrid polymer–nanometal lightweight structures5 February 2019 | Aerospace Systems, Vol. 2, No. 2A Fully Coupled Body Force-Engine Performance Methodology For Boundary Layer IngestionLuis López de Vega, Guillaume Dufour and Nicolás García Rosa16 August 2019A Fault Management-Oriented Early-Design Framework for Electrical Propulsion Aircraft1 Jun 2019 | IEEE Transactions on Transportation Electrification, Vol. 5, No. 2The Effect of Incoming Boundary Layer Characteristics On The Performance Of a Distributed Propulsion SystemPuja Upadhyay and Khairul Q. Zaman6 January 2019Conceptual Design of a BLI Propulsor Capturing Aero-Propulsive Coupling and Distortion ImpactsManish Pokhrel, Mingxuan Shi, Jai Ahuja, Jonathan Gladin and Dimitri N. Mavris6 January 2019Model Fidelity Requirements in Boundary Layer Ingestion Propulsion System Conceptual DesignMingxuan Shi, Manish Pokhrel, Jonathan Gladin, Elena Garcia and Dimitri N. Mavris24 June 2018Optimal Approximations of Coupling in Multidisciplinary ModelsRicardo Baptista, Youssef Marzouk, Karen Willcox and Benjamin Peherstorfer31 May 2018 | AIAA Journal, Vol. 56, No. 6Convergent Nozzle Gross Thrust Coefficient and Discharge Coefficient Calculation with Boundary Layer Ingestion (BLI) EffectsMingxuan Shi, Manish Pokhrel, Jonathan C. Gladin, Elena Garcia and Dimitri N. Mavris7 July 2017Simultaneous Propulsion System and Trajectory OptimizationEric S. Hendricks, Robert D. Falck and Justin S. Gray2 June 2017 What's Popular 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 9 - 13 January 2017Grapevine, Texashttps://doi.org/10.2514/6.2017-1753 CrossmarkInformationThis material is declared a work of the U.S. Government and is not subject to copyright protection in the United States. TopicsAerodynamic PerformanceAerodynamicsAerospace SciencesAirbreathing Jet EngineAircraft EnginesBoundary LayersElectric PropulsionFluid DynamicsFluid Flow PropertiesFluid MechanicsPropulsion and PowerShock WavesSpacecraft PropulsionVortex Dynamics KeywordsBoundary LayersOverall Propulsive EfficiencyAircraft ConfigurationsAerodynamic Shape OptimizationMultidisciplinary Design OptimizationElectric PropulsionThermodynamic CyclesAerodynamic PerformanceMass Flow RateStatic PressureDigital Topics Multidisciplinary Design Optimization