LEADER 01419cam a2200301 i 4500
001 991001701809707536
005 20030702182755.0
008 920603s1991    gw       b    000 0 ger  
035   $ab12184895-39ule_inst
040   $aBiblioteca Interfacoltà$bita
041   $ager
082 0 $a193
100 1 $aHeidegger, Martin$010351
245 14$aDie Metaphysik des deutschen Idealismus :$bzur erneuten Auslegung von Schelling : philosophische Untersuchungen über das Wesen der menschlichen Freiheit und die damit zusammenhängenden Gegenstände (1809) /$cMartin Heidegger
260   $aFrankfurt am Main :$bKlostermann,$cc1991
300   $aIX, 209 p. ;$c21 cm
440  0$aGesamtausgabe ;$vBd. 49. Abt. 2., Vorlesungen 1919-1944
500   $aSul verso: "Freiburger Vorlesung I. Trimester 1941, Freiburger Seminar Sommersemester 1941" hrsg. von Günter Seubold
504   $aInclude referenze bibliografiche
600 10$aSchelling, Friedrich Wilhelm Joseph :$cvon$d<1775-1854>
650  0$aIdealismo
700 1 $aSeubold, Günter$d<1955- >
907   $a.b12184895$b02-04-14$c03-07-03
912   $a991001701809707536
945   $aLE002 Fil. XVII 1/049    $cv. 49    $g1$i2002000288301    $lle002$n[ed. 1991]    $op$pE0.00$q-$rn$so  $t0$u0$v0$w0$x0$y.i12548340$z15-07-03
996   $aMetaphysik des deutschen Idealismus$9145800
997   $aUNISALENTO
998   $ale002$b03-07-03$cm$da  $e-$fger$ggw $h4$i1

LEADER 01831nam  2200481   450 
001 9910706120203321
005 20170914100726.0
035   $a(CKB)5470000002455228
035   $a(OCoLC)1003643373
035   $a(EXLCZ)995470000002455228
100   $a20170914j199912    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSubsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration /$fBryan A. Campbell [and three others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 1999.
215   $a1 online resource (103 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209701
300   $a"December 1999."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 102-103 ).
606   $aSubsonic wind tunnels$2nasat
606   $aLeading edge flaps$2nasat
606   $aVortices$2nasat
606   $aSupersonic transports$2nasat
606   $aAerodynamic configurations$2nasat
606   $aSeparated flow$2nasat
615  7$aSubsonic wind tunnels.
615  7$aLeading edge flaps.
615  7$aVortices.
615  7$aSupersonic transports.
615  7$aAerodynamic configurations.
615  7$aSeparated flow.
700   $aCampbell$b Bryan A.$01395236
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706120203321
996   $aSubsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration$93453410
997   $aUNINA