Volume 16, Issue 4 No AccessPrediction of Roll Controllability of Slender Cruciform Canard ConfigurationsI. Gur, J. Shinar, and J. RomI. Gur, J. Shinar and J. RomI. Gur Technion —Israel Institute of Technology, Haifa, IsraelSearch for more papers by this author, J. Shinar Technion —Israel Institute of Technology, Haifa, IsraelSearch for more papers by this author and J. Rom Technion —Israel Institute of Technology, Haifa, IsraelSearch for more papers by this authorPublished Online:23 May 2012https://doi.org/10.2514/3.57650SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous article Next article FiguresReferencesRelatedDetailsSee PDF for referencesCited byTheoretical prediction of roll moment on wing-controlled missile Sadao Akishita , Ryujiro Kurosaki , Kanzo Okada and Tomoji Hirata 22 May 2012 | Journal of Aircraft, Vol. 23, No. 11 What's Popular Volume 16, Number 4July 1979 Metrics Crossmark TopicsAerodynamic PerformanceAerodynamicsAerospace SciencesAircraft DesignAircraft Operations and TechnologyAircraft Stability and ControlAircraft Wing DesignComputational Fluid DynamicsFinite Element MethodFlight Control SurfacesFluid DynamicsSlip (Aerodynamics)Vortex DynamicsWind Tunnels KeywordsWing Body CombinationVortex ModelingAngle of AttackAerodynamic CharacteristicsControl SurfacesMathematical ModelsSupersonic Wind TunnelsAspect RatioCruciform TailSlender Body TheoryDigital Published online23 May 2012