LEADER 01115cam0-2200361---450-
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010   $a2-84050-247-X
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100   $a19990604d2002----km-y0itay50------ba
101 0 $afre
102   $aFR
105   $a--------001yy
200 1 $aÉtudes sur les illuminations de Rimbaud$fSergio Sacchi$gtextes recueillis par Olivier Bivort, André Guyaux et Mario Matucci
210   $aParis$cPresses de l'université de Paris-Sorbonne$d2002
215   $a266 p.$d21 cm
225 1 $aMémoire de la critique
610 0 $aRimbaud, Arthur$aIlluminations
676   $a841.8
700  1$aSacchi,$bSergio$0176703
702  1$aBivort,$bOlivier
702  1$aGuyaux,$bAndré
702  1$aMatucci,$bMario$f<1920->
801  0$aIT$bUNINA$gRICA$2UNIMARC
901   $aBK
912   $a990004391070403321
952   $a841.8 RIMB/S 2$bDip.f.m.11994$fFLFBC
959   $aFLFBC
996   $aÉtudes sur les illuminations de Rimbaud$9542382
997   $aUNINA

LEADER 02021oam  2200577Ka 450 
001 9910698995003321
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035   $a(CKB)5470000002397921
035   $a(OCoLC)384172382
035   $a(EXLCZ)995470000002397921
100   $a20090610d1989      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFeasibility and benefits of laminar flow control on supersonic cruise airplanes$b[electronic resource] /$fA.G. Powell, S. Agrawal, T. R. Lacey
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[1989]
215   $a1 volume
225 1 $aNASA contractor report ;$v181817
300   $aTitle from title screen (viewed Jun. 9, 2009)
606   $aAerodynamic configurations$2nasat
606   $aBoundary layer control$2nasat
606   $aBoundary layer stability$2nasat
606   $aFeasibility analysis$2nasat
606   $aFighter aircraft$2nasat
606   $aLaminar boundary layer$2nasat
606   $aLaminar flow$2nasat
606   $aSupersonic aircraft$2nasat
606   $aSupersonic cruise aircraft research$2nasat
606   $aSupersonic transports$2nasat
615  7$aAerodynamic configurations.
615  7$aBoundary layer control.
615  7$aBoundary layer stability.
615  7$aFeasibility analysis.
615  7$aFighter aircraft.
615  7$aLaminar boundary layer.
615  7$aLaminar flow.
615  7$aSupersonic aircraft.
615  7$aSupersonic cruise aircraft research.
615  7$aSupersonic transports.
700   $aPowell$b A. G$01389264
701   $aAgrawal$b Sudhir$0515084
701   $aLacey$b T. R$01389265
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910698995003321
996   $aFeasibility and benefits of laminar flow control on supersonic cruise airplanes$93440557
997   $aUNINA