LEADER 00927nam a22002531i 4500
001 991004125109707536
005 20031004093922.0
008 031111s1969    gw a||||||||||||||||ger  
035   $ab12525571-39ule_inst
035   $aARCHE-055884$9ExL
040   $aDip.to Lingue$bita$cA.t.i. Arché s.c.r.l. Pandora Sicilia s.r.l.
082 04$a809.9145
100 1 $aKlessmann, Eckart$0175628
245 14$aDie Welt der Romantik /$cEckart Klessmann
260   $aMünchen :$bKurt Desch,$c1969
300   $a367 p. :$bill. ;$c29 cm
440  0$aGrosse Kulturepochen in Texten, Bildern und Zeugnissen
650  4$aRomanticismo
907   $a.b12525571$b02-04-14$c13-11-03
912   $a991004125109707536
945   $aLE012 F.G. 430$g1$i2012000060111$lle012$o-$pE0.00$q-$rl$s-  $t0$u0$v0$w0$x0$y.i12967841$z13-11-03
996   $aWelt der Romantik$9184234
997   $aUNISALENTO
998   $ale012$b13-11-03$cm$da  $e-$fger$ggw $h4$i1

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