No AccessMode splitting in an inflated polyimide cylinder with circumferential asymmetryKara Slade, Lawrence Virgin and Michael TinkerKara SladeNASA, Langley Research Center, Hampton, VASearch for more papers by this author, Lawrence VirginDuke Univ., Durham, NCSearch for more papers by this author and Michael TinkerNASA, Marshall Space Flight Center, Huntsville, ALSearch for more papers by this authorPublished Online:22 Aug 2012https://doi.org/10.2514/6.2001-1411SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byRigidizable Inflatable Get-Away-Special Experiment Space Flight Data Analysis Jonathan T. Black , Richard G. Cobb , Eric D. Swenson and Brett J. Cooper 23 May 2012 | Journal of Spacecraft and Rockets, Vol. 48, No. 3Structural dynamics experimental activities in ultra-lightweight and inflatable space structuresRichard Pappa, John Lassiter and Brian Ross22 August 2012 What's Popular 19th AIAA Applied Aerodynamics Conference 11 June 2001 - 14 June 2001Anaheim,CA,U.S.A.https://doi.org/10.2514/6.2001-1411 Crossmark TopicsBeam (Structures)Computational Fluid DynamicsFinite Element MethodFinite Element SoftwareFlexible and Active StructuresFluid DynamicsMechanical and Structural VibrationsShell StructuresStructural AnalysisStructural EngineeringStructures, Design and TestVibration Measuring Instruments KeywordsFinite Element ModelingInflatable StructuresThin FilmsNASA Marshall Space Flight CenterBeam (Structures)Inflatable Antenna ExperimentShuttle Remote Manipulator SystemSolar Thermal PropulsionNastranCommunications AntennaDigital Topics Applied Aerodynamics