No AccessA Multi-Fidelity Prediction of Aerodynamic and Sonic Boom Characteristics of the JAXA Wing BodyForrest L. Carpenter, Paul Cizmas, Christian R. Bolander, Ted N. Giblette and Douglas F. HunsakerForrest L. CarpenterTexas A&M UniversitySearch for more papers by this author, Paul CizmasTexas A&M UniversitySearch for more papers by this author, Christian R. BolanderUtah State UniversitySearch for more papers by this author, Ted N. GibletteUtah State UniversitySearch for more papers by this author and Douglas F. HunsakerUtah State UniversitySearch for more papers by this authorAIAA 2019-3237Session: Aerodynamic Design/Shape Optimization IIPublished Online:14 Jun 2019https://doi.org/10.2514/6.2019-3237SectionsPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byA Multi-Objective Hybrid Optimization Methodology for Minimizing Aircraft Sonic Boom and Drag at Fixed LiftAnn-Kayana Blanchard, Justin Schoppe, Sohail Reddy, George S. Dulikravich and Paul G. Cizmas29 December 2021UNS3D Near-Field Predictions for the Third AIAA Sonic Boom Prediction WorkshopForrest L. Carpenter , Jackson Kassing and Paul G. A. Cizmas31 August 2021 | Journal of Aircraft, Vol. 0, No. 0Implementation of Multidisciplinary Multi-Fidelity Uncertainty Quantification Methods in Sonic Boom PredictionHuseyin E. Tekaslan, Sihmehmet Yildiz, Yusuf Demiroglu and Melike Nikbay28 July 2021Exploration of Optimal Propulsion System Airframe Integration Design Concepts for a Low Boom Supersonic AircraftRumed Imrak, Emre Karaselvi, Bulent Tutkun and Melike Nikbay28 July 2021Multi-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape DesignYusuf Demiroglu, Sihmehmet Yildiz and Melike Nikbay4 January 2021UNS3D Simulations for the Third Sonic Boom Prediction Workshop Part II: C608 Low-Boom Flight DemonstratorForrest L. Carpenter and Paul Cizmas8 June 2020UNS3D Simulations for the Third Sonic Boom Prediction Workshop Part I: Biconvex 9×7 Shock-Plume Interaction ModelJackson Kassing, Forrest L. Carpenter and Paul Cizmas8 June 2020 What's Popular AIAA Aviation 2019 Forum 17-21 June 2019Dallas, Texashttps://doi.org/10.2514/6.2019-3237 CrossmarkInformationCopyright © 2019 by Forrest L. Carpenter IV. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamicsAeronautical EngineeringAeronauticsBoundary LayersComputational Fluid DynamicsConservation of Momentum EquationsEquations of Fluid DynamicsFlow RegimesFluid DynamicsFluid Flow PropertiesNumerical AnalysisShock WavesVortex Dynamics KeywordsSonic BoomsAerodynamic FlowsRoe Approximate Riemann SolverAerodynamic CoefficientsAircraft ConfigurationsWing RootComputational Fluid DynamicsSupersonic AircraftFlow SeparationAerodynamic Flow Properties Topics Multidisciplinary Design Optimization