LEADER 01021nam0-22003371i-450- 001 990002054590403321 005 20021010 035 $a000205459 035 $aFED01000205459 035 $a(Aleph)000205459FED01 035 $a000205459 100 $a20021010d--------km-y0itay50------ba 101 0 $aita 200 1 $a<>zoologie agricole$eouvrage comprenant l' histoire entiere des animaux nuisibles et des animaux utiles$fEmile Blanchard 210 $aParis$cV. Masson$ds.d. 215 $a192 p. 47 tv. col.$d32 cm 300 $aOpera incompleta di tavole 610 0 $aZoologia Agraria 610 0 $aPiante Ornamentali, Insetti 610 0 $aPiante Ornamentali, Entomologia 610 0 $aFiori 676 $a590$a595.7$a635.9 700 1$aBlanchard,$bÉmile$f<1819-1900>$0353439 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990002054590403321 952 $a61 VIII A.5/01$b409$fDAGEN 959 $aDAGEN 996 $aZoologie agricole$9367687 997 $aUNINA DB $aING01 LEADER 02284nam 2200589I 450 001 9910707239903321 005 20160621153028.0 035 $a(CKB)5470000002463110 035 $a(OCoLC)951986585 035 $a(EXLCZ)995470000002463110 100 $a20160621j199605 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 13$aAn aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation /$fW. Keats Wilkie, K.C. Park 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMay 1996. 215 $a1 online resource (iv, 58 pages)$cillustrations 225 1 $aNASA technical memorandum ;$v110252 300 $aTitle from title screen (viewed June 21, 2016). 300 $a"May 1996." 300 $a"Performing organization: NASA Langley Research Center, Hampton, VA and Vehicle Structures Directorate, U.S. Army Research Laboratory, NASA Langley Research Center, Hampton,VA"--Report documentation page. 300 $a"ARL-MR-328." 320 $aIncludes bibliographical references (pages 22-24). 606 $aAeroelasticity$2nasat 606 $aHelicopters$2nasat 606 $aFiber composites$2nasat 606 $aRotary wings$2nasat 606 $aUnsteady aerodynamics$2nasat 606 $aDifferential equations$2nasat 606 $aGalerkin method$2nasat 606 $aNumerical integration$2nasat 615 7$aAeroelasticity. 615 7$aHelicopters. 615 7$aFiber composites. 615 7$aRotary wings. 615 7$aUnsteady aerodynamics. 615 7$aDifferential equations. 615 7$aGalerkin method. 615 7$aNumerical integration. 700 $aWilkie$b W. Keats$01410623 702 $aPark$b K. C. 712 02$aU.S. Army Research Laboratory. 712 02$aLangley Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910707239903321 996 $aAn aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation$93499760 997 $aUNINA