No AccessRolling airframe missile aerodynamic predictions using a chimera approach for dithering canardsL. HallL. HallDynetics, Inc., Huntsville, ALSearch for more papers by this authorPublished Online:22 Aug 2012https://doi.org/10.2514/6.2002-405SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byCFD Validation of Interaction of Fin Trailing Vortex with Downstream Control Surface in High Subsonic FlowJames DeSpirito2 January 2016Theoretical analysis of direct-finding targets with rolling-airframe passive radar by phase interference technique1 Oct 2006Aerodynamic Analysis of a Spinning Missile with Dithering Canards Tor A. Nygaard and Robert L. Meakin 13 December 2011 | Journal of Spacecraft and Rockets, Vol. 41, No. 5Numerical Simulation of Rolling Airframes Using a Multilevel Cartesian Method Scott M. Murman , Michael J. Aftosmis and Marsha J. Berger 23 May 2012 | Journal of Spacecraft and Rockets, Vol. 41, No. 3Numerical Simulation of Rolling Airframes Using a Multi-Level Cartesian MethodScott Murman, Michael Aftosmis and Marsha Berger25 June 2012Chimera Moving Body Methodology for Rolling Airframe Missile Simulation with Dithering CanardsLes Hall25 June 2012 What's Popular 40th AIAA Aerospace Sciences Meeting & Exhibit 14 January 2002 - 17 January 2002Reno,NV,U.S.A.https://doi.org/10.2514/6.2002-405 Crossmark TopicsAerodynamic PerformanceAerodynamicsAerospace SciencesAircraft Components and StructureAircraft DesignAircraft Operations and TechnologyAircraft Stability and ControlAircraft Wing DesignFlight Control SurfacesFluid DynamicsTurbulenceTurbulence ModelsVortex DynamicsWind Tunnels KeywordsAirframesSpinning MissileCanardAerodynamic CoefficientsWind Tunnel TestsControl SurfacesAngle of AttackVorticesAeronauticsReynolds Averaged Navier StokesDigital Topics Aerospace Systems, Operations and Life Cycle