LEADER 01621nam  2200457I  450 
001 9910705715403321
005 20170706144755.0
035   $a(CKB)5470000002453257
035   $a(OCoLC)992978545
035   $a(EXLCZ)995470000002453257
100   $a20170706j201609    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExtracting damping ratio from dynamic data and numerical solutions /$fM.J. Casiano
210  1$aHuntsville, Alabama :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$dSeptember 2016.
215   $a1 online resource (vii, 29 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2016-218227
300   $a"September 2016."
300   $a"Performing organization: George C. Marshall Space Flight Center"--Report documentation page.
320   $aIncludes bibliographical references (page 29).
606   $aAutocorrelation$2nasat
606   $aDamping$2nasat
606   $aDynamic models$2nasat
606   $aFinite element method$2nasat
606   $aSoftware development tools$2nasat
615  7$aAutocorrelation.
615  7$aDamping.
615  7$aDynamic models.
615  7$aFinite element method.
615  7$aSoftware development tools.
700   $aCasiano$b M. J.$01388631
712 02$aGeorge C. Marshall Space Flight Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705715403321
996   $aExtracting damping ratio from dynamic data and numerical solutions$93487234
997   $aUNINA