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100   $a20111115j198912    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA transient response method for linear coupled substructures /$fJ.R. Admire and J.A. Brunty
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,$dDecember 1989.
215   $a1 online resource (v, 20 pages) $cillustrations
225 1 $aNASA technical paper ;$v2926
300   $a"December 1989"--Report documentation page
300   $a"Performing organization: George C. Marshall Space Flight Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 19-20).
606   $aDiscrete functions$2nasat
606   $aLinear systems$2nasat
606   $aLoads (forces)$2nasat
606   $aMathematical models$2nasat
606   $aNumerical integration$2nasat
606   $aTransient response$2nasat
615  7$aDiscrete functions.
615  7$aLinear systems.
615  7$aLoads (forces)
615  7$aMathematical models.
615  7$aNumerical integration.
615  7$aTransient response.
700   $aAdmire$b J. R.$01395496
702   $aBrunty$b J. A.
712 02$aGeorge C. Marshall Space Flight Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Division (1987-1990 ),
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910705755203321
996   $aA transient response method for linear coupled substructures$93454109
997   $aUNINA