LEADER 01059nam a2200277 i 4500
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008 991203s1993    it            ||| | ita  
020   $a8813180276
035   $ab11591419-39ule_inst
035   $aLE02728380$9ExL
040   $aDip.to Studi Giuridici$bita
082 0 $a341.78
084   $aPR-X/A
100 1 $aSalerno, Francesco$0229778
245 13$aLa giurisdizione italiana in materia cautelare /$cFrancesco Salerno
260   $aPadova :$bCEDAM,$c1993
300   $axv, 474 p. ;$c24 cm.
490 0 $aStudi e pubblicazioni della Rivista di diritto internazionale privato e processuale ;$v40
650  4$aProvvedimenti cautelari$xConvenzioni internazionali
907   $a.b11591419$b01-03-17$c02-07-02
912   $a991001977039707536
945   $aLE027 341.78 SAL01.01$g1$i2027000003853$lle027$o-$pE0.00$q-$rl$s-  $t0$u4$v1$w4$x0$y.i11801463$z02-07-02
996   $aGiurisdizione italiana in materia cautelare$9689170
997   $aUNISALENTO
998   $ale027$b01-01-99$cm$da  $e-$fita$git $h3$i1

LEADER 02021oam  2200577Ka 450 
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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