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100   $a--------d--------km-y0itay50------ba
101 0 $aeng
200 1 $a<<The >>theory of Viscoelasticity$fby Bland
210   $aLondon [etc.]$cPergamon Press$d1960
225 1 $aInternational series of monographs on pure and applied mathematics
300   $a10mo Vol.
700  1$aBland,$bDavid Russel$044945
801  0$aIT$bUNINA$gRICA$2UNIMARC
901   $aBK
912   $a990001136510403321
952   $aC-37-(10$b3423$fMA1
959   $aMA1
996   $aTheory of Viscoelasticity$9345204
997   $aUNINA

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100   $a20160721j201604    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCompressive testing of stitched frame and stringer alternate configurations /$fFrank A. Leone, Jr., Dawn C. Jegley
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dApril 2016.
215   $a1 online resource (iv, 27 pages)$ccolor illustrations
225 1 $aNASA/TM ;$v2016-218974
300   $aTitle from title screen (viewed July 21, 2016).
300   $a"April 2016."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 26-27).
606   $aBody-wing configurations$2nasat
606   $aComposite structures$2nasat
606   $aFuselages$2nasat
606   $aStringers$2nasat
606   $aTransport aircraft$2nasat
615  7$aBody-wing configurations.
615  7$aComposite structures.
615  7$aFuselages.
615  7$aStringers.
615  7$aTransport aircraft.
700   $aLeone$b Frank A.$01399025
702   $aJegley$b Dawn C.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707343903321
996   $aCompressive testing of stitched frame and stringer alternate configurations$93493999
997   $aUNINA