No AccessStudies on Fluidic Injection Thrust Vectoring in Aerospike NozzlesK. Hanumanthrao, S. Ragothaman, B. Arun Kumar, M. Giri Prasad and V. Sanal KumarK. HanumanthraoKumaraguru College of TechnologySearch for more papers by this author, S. RagothamanKumaraguru College of TechnologySearch for more papers by this author, B. Arun KumarKumaraguru College of TechnologySearch for more papers by this author, M. Giri PrasadKumaraguru College of TechnologySearch for more papers by this author and V. Sanal KumarKumaraguru College of TechnologySearch for more papers by this authorPublished Online:14 Jun 2012https://doi.org/10.2514/6.2011-293SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byTechniques of Fluidic Thrust Vectoring in Jet Engine Nozzles: A Review31 July 2023 | Energies, Vol. 16, No. 15Fluidic Thrust Vectoring for Annular Aerospike NozzleMichele Ferlauto, Andrea Ferrero and Roberto Marsilio17 August 2020Numerical investigation of injection angle effects on shock vector control performance31 October 2017 | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 233, No. 2 What's Popular 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 04 January 2011 - 07 January 2011Orlando, Floridahttps://doi.org/10.2514/6.2011-293 Crossmark TopicsAerodynamicsAerospace SciencesComputational Fluid DynamicsConservation of Momentum EquationsEquations of Fluid DynamicsFinite Volume MethodFlow RegimesFluid DynamicsFluid Flow PropertiesNumerical AnalysisRocket EngineRocketry KeywordsRocket Engine NozzleThrust Vector ControlReusable Launch VehicleRocket Nozzle FlowFlow CharacteristicsNavier Stokes EquationsFinite Volume SchemeBell Shaped NozzlePropulsion and PowerRocketsDigital Topics Aerospace Systems, Operations and Life Cycle