LEADER 01129nam a22002651i 4500
001 991000190169707536
005 20040729150908.0
008 040802s1929    fr |||||||||||||||||fre  
035   $ab13188161-39ule_inst
035   $aARCHE-114077$9ExL
040   $aBiblioteca Interfacoltà$bita$cA.t.i. Arché s.c.r.l. Pandora Sicilia s.r.l.
082 04$a842.7
100 1 $aVigny, Alfred :$cde$0172892
245 10$aThéatre complet /$cAlfred De Vigny ; remarques et notes par M. Auguste Dorchain
260   $aParis :$bLibraire Garnier Freres,$c1929-
300   $av. ;$c19 cm
440  0$aSelecta des classiques Garnier
700 1 $aDorchain, Auguste
907   $a.b13188161$b02-04-14$c05-08-04
912   $a991000190169707536
945   $aLE002 Fondo Giudici L 886/001$g1$i2002000334275$lle002$nV. 1. - C. 1$o-$pE0.00$q-$rn$so  $t0$u0$v0$w0$x0$y.i1383034x$z05-08-04
945   $aLE002 Fondo Giudici L 886/002$g1$i2002000334282$lle002$nV. 2. - C. 1$o-$pE0.00$q-$rn$so  $t0$u0$v0$w0$x0$y.i13830351$z05-08-04
996   $aThéâtre complet$91045925
997   $aUNISALENTO
998   $ale002$b05-08-04$cm$da  $e-$ffre$gfr $h0$i2

LEADER 01950oam  2200577   450 
001 9910716863203321
005 20210924135235.0
035   $a(CKB)5470000002525553
035   $a(OCoLC)1159597682
035   $a(EXLCZ)995470000002525553
100   $a20200623d1938      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFatigue testing of wing beams by the resonance method /$fby William M. Bleakney
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1938.
215   $a1 online resource (22 pages, 24 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 660
300   $a"August 1938."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 22).
606   $aAirplanes$xWings$xTesting
606   $aAluminum alloys
606   $aAlloys$xFatigue$xTesting
606   $aLoads (Mechanics)
606   $aAirplanes$xWings$xTesting$2fast
606   $aAlloys$xFatigue$xTesting$2fast
606   $aAluminum alloys$2fast
606   $aLoads (Mechanics)$2fast
615  0$aAirplanes$xWings$xTesting.
615  0$aAluminum alloys.
615  0$aAlloys$xFatigue$xTesting.
615  0$aLoads (Mechanics)
615  7$aAirplanes$xWings$xTesting.
615  7$aAlloys$xFatigue$xTesting.
615  7$aAluminum alloys.
615  7$aLoads (Mechanics)
700   $aBleakney$b William M.$01402985
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910716863203321
996   $aFatigue testing of wing beams by the resonance method$93474640
997   $aUNINA