02085nam 2200553Ia 450 991069706300332120230902162105.0(CKB)5470000002384271(OCoLC)653244223(EXLCZ)99547000000238427120100806d2009 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierFlutter sensitivity to boundary layer thickness, structural damping, and static pressure differential for a shuttle tile overlay repair concept[electronic resource] /Robert C. Scott and Robert E. BartelsHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2009]1 online resource (30 pages) illustrations (some color)NASA/TM ;2009-215708Title from PDF title screen (viewed Aug. 6, 2010)."April 2009."Includes bibliographical references (pages 21-22).NASA technical memorandum ;2009-215708.AeroelasticitynasatBoundary layersnasatComputational fluid dynamicsnasatDynamic structural analysisnasatSpace shuttlesnasatStructural vibrationnasatTilesnasatVibration dampingnasatAeroelasticity.Boundary layers.Computational fluid dynamics.Dynamic structural analysis.Space shuttles.Structural vibration.Tiles.Vibration damping.Scott Robert C6557Bartels Robert E106924Langley Research Center.GPOGPOBOOK9910697063003321Flutter sensitivity to boundary layer thickness, structural damping, and static pressure differential for a shuttle tile overlay repair concept3467339UNINA