LEADER 01215nam a2200313 i 4500
001 991000565019707536
005 20020506132331.0
008 001103s1965    it            ||| | ita  
035   $ab1071876x-39ule_inst
035   $aEXGIL147815$9ExL
040   $aBiblioteca Interfacoltà$bita
082 04$a709.45
082 04$a927
100 1 $aPascoli, Lione$d<1674-1744>$0215146
245 10$aVite de' pittori, scultori, ed architetti moderni :$bcon indice analitico /$cLione Pascoli
250   $aRist. anast.
260   $aRoma :$bSOMU,$c1965
300   $a2 v. ;$c24 cm.
490 0 $aFonti per la storia dell'arte ;$v2
500   $aRipr. facs. dell'ed.: Roma, 1730-1736
907   $a.b1071876x$b23-02-17$c28-06-02
912   $a991000565019707536
945   $aLE002 SB 927 PAS
945   $aLE002 Ar. I G 12/I$cV. 1$g1$i2002000742070$lle002$o-$pE0.00$q-$rn$so  $t0$u0$v0$w0$x0$y.i10815478$z28-06-02
945   $aLE002 SB 927 PAS
945   $aLE002 Ar. I G 12/II$cV. 2$g1$i2002000742087$lle002$o-$pE0.00$q-$rn$so  $t0$u0$v0$w0$x0$y.i1081548x$z28-06-02
996   $aVite de' pittori, scultori, ed architetti moderni$9268950
997   $aUNISALENTO
998   $ale002$b01-01-00$cm$da  $e-$fita$git $h0$i2

LEADER 01708nam  2200481Ia 450 
001 9910700760003321
005 20110802115728.0
035   $a(CKB)5470000002411406
035   $a(OCoLC)744424123
035   $a(EXLCZ)995470000002411406
100   $a20110802d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aEquivalent longitudinal area distributions of the B-58 and XB-70-1 airplanes for use in wave drag and sonic boom calculations$b[electronic resource] /$fAna F. Tinetti ... [and others]
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2011]
215   $a1 online resource (29 pages) $cillustrations
225 1 $aNASA/CR ;$v2011-217078
300   $aTitle from title screen (viewed on Aug. 2, 2011).
300   $a"March 2011."
320   $aIncludes bibliographical references (pages 11-12).
606   $aWave drag$2nasat
606   $aSonic booms$2nasat
606   $aB-58 aircraft$2nasat
606   $aDelta wings$2nasat
606   $aDrag measurement$2nasat
606   $aMach number$2nasat
615  7$aWave drag.
615  7$aSonic booms.
615  7$aB-58 aircraft.
615  7$aDelta wings.
615  7$aDrag measurement.
615  7$aMach number.
701   $aTinetti$b Ana F$01395871
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700760003321
996   $aEquivalent longitudinal area distributions of the B-58 and XB-70-1 airplanes for use in wave drag and sonic boom calculations$93455053
997   $aUNINA