LEADER 01712nam  2200505I  450 
001 9910702734303321
005 20150203131956.0
035   $a(CKB)5470000002430858
035   $a(OCoLC)902680688
035   $a(EXLCZ)995470000002430858
100   $a20150203j201409    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAeroelastic tailoring via tow steered composites /$fBret K. Stanford, Christine V. Jutte
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dSeptember 2014.
215   $a1 online resource (25 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2014-218517
300   $aTitle from title screen (viewed Feb. 3, 2015).
300   $a"September 2014."
320   $aIncludes bibliographical references (pages 24-25).
606   $aAeroelasticity$2nasat
606   $aLaminates$2nasat
606   $aStiffness matrix$2nasat
606   $aTransverse loads$2nasat
606   $aHigh aspect ratio$2nasat
606   $aAerodynamic loads$2nasat
615  7$aAeroelasticity.
615  7$aLaminates.
615  7$aStiffness matrix.
615  7$aTransverse loads.
615  7$aHigh aspect ratio.
615  7$aAerodynamic loads.
700   $aStanford$b Bret K.$01405266
702   $aJutte$b Christine V.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702734303321
996   $aAeroelastic tailoring via tow steered composites$93542440
997   $aUNINA