LEADER 01339nam a22003011i 4500 001 991001686829707536 005 20031202165321.0 008 040407s1969 it |||||||||||||||||ita 035 $ab12808337-39ule_inst 035 $aARCHE-078796$9ExL 040 $aDip.to Scienze Storiche$bita$cA.t.i. Arché s.c.r.l. Pandora Sicilia s.r.l. 082 04$a945.083072 100 1 $aMaturi, Walter$0183121 245 10$aInterpretazioni del Risorgimento :$blezioni di storia della storiografia /$cWalter Maturi ; prefazione di Ernesto Sestan ; aggiornamento bibliografico di Rosario Romeo 250 $a3. ed. 260 $aTorino :$bEinaudi,$cc1962 300 $aXXIV, 808 p. ;$c22 cm 440 0$aBiblioteca di cultura storica ;$v72 650 4$aRisorgimento italiano$xStoriografia 700 1 $aRomeo, Rosario 700 1 $aSestan, Ernesto 907 $a.b12808337$b13-10-21$c16-04-04 912 $a991001686829707536 945 $aLE009 STOR.63-136$g1$i2009000212794$lle009$o-$pE0.00$q-$rl$s- $t0$u2$v0$w2$x0$y.i1335632x$z16-04-04 945 $aLE023 945.083 MAT 1 1$g2$i2009000212800$lle023$nLE009 STOR.63-136/bis (vecchia collocazione) $o-$pE0.00$q-$rl$s- $t0$u0$v0$w0$x0$y.i13356331$z16-04-04 996 $aInterpretazioni del Risorgimento$9155300 997 $aUNISALENTO 998 $ale009$ale023$b16-04-04$cm$da $e-$fita$git $h0$i2 LEADER 02173oam 2200661 450 001 9910716066503321 005 20210908083152.0 035 $a(CKB)5470000002517438 035 $a(OCoLC)785280910$z(OCoLC)48181155$z(OCoLC)761258706 035 $a(OCoLC)995470000002517438 035 $a(EXLCZ)995470000002517438 100 $a20120408j196901 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aPerformance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions /$fby Helmut F. Butze, Arthur M. Trout, and Harry M. Moyer 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dJanuary 1969. 215 $a1 online resource (ii, 25 pages) $cillustrations 225 1 $aNASA/TN ;$vD-4996 300 $a"January 1969." 320 $aIncludes bibliographical references (page 25). 606 $aAerodynamics$2nasat 606 $aCombustion chambers$2nasat 606 $aAerodynamics, Supersonic 606 $aAirplanes$xTurbojet engines 606 $aAerodynamics, Supersonic$2fast 606 $aAirplanes$xTurbojet engines$2fast 606 $aCombustion chambers$2fast 615 7$aAerodynamics. 615 7$aCombustion chambers. 615 0$aAerodynamics, Supersonic. 615 0$aAirplanes$xTurbojet engines. 615 7$aAerodynamics, Supersonic. 615 7$aAirplanes$xTurbojet engines. 615 7$aCombustion chambers. 700 $aButze$b Helmut F.$01413653 702 $aTrout$b Arthur M. 702 $aMoyer$b Harry M. 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bOCLCE 801 1$bOCLCE 801 2$bTRL 801 2$bAD# 801 2$bOCLCQ 801 2$bOCLCO 801 2$bOCLCF 801 2$bOCLCQ 801 2$bCOP 801 2$bGPO 801 2$bOCLCO 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910716066503321 996 $aPerformance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions$93510513 997 $aUNINA