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100   $a20100806d2009      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFlutter sensitivity to boundary layer thickness, structural damping, and static pressure differential for a shuttle tile overlay repair concept$b[electronic resource] /$fRobert C. Scott and Robert E. Bartels
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2009]
215   $a1 online resource (30 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2009-215708
300   $aTitle from PDF title screen (viewed Aug. 6, 2010).
300   $a"April 2009."
320   $aIncludes bibliographical references (pages 21-22).
410  0$aNASA technical memorandum ;$v2009-215708.
606   $aAeroelasticity$2nasat
606   $aBoundary layers$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aDynamic structural analysis$2nasat
606   $aSpace shuttles$2nasat
606   $aStructural vibration$2nasat
606   $aTiles$2nasat
606   $aVibration damping$2nasat
615  7$aAeroelasticity.
615  7$aBoundary layers.
615  7$aComputational fluid dynamics.
615  7$aDynamic structural analysis.
615  7$aSpace shuttles.
615  7$aStructural vibration.
615  7$aTiles.
615  7$aVibration damping.
700   $aScott$b Robert C$06557
701   $aBartels$b Robert E$0106924
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697063003321
996   $aFlutter sensitivity to boundary layer thickness, structural damping, and static pressure differential for a shuttle tile overlay repair concept$93467339
997   $aUNINA