LEADER 01398nam--2200445---450- 001 990000707550203316 005 20041228113736.0 010 $a88-15-05482-0 035 $a0070755 035 $aUSA010070755 035 $a(ALEPH)000070755USA01 035 $a0070755 100 $a20011025d1996----km-y0itay0103----ba 101 $aita 102 $aIT 105 $a||||||||001yy 200 1 $aReligione e memoria$fDaniele Hervieu-Leger$g[traduzione di Aldo Pasquali] 210 $aBologna$cIl mulino$d1996 215 $a278 p.$d22 cm 225 2 $aSaggi$v448 312 $aLa religion pour mémoire 410 $12001$aSaggi$v448 454 $12001$aLa religion pour mémoire$936567 606 0 $aReligione e società$zSec. 20. 676 $a306.6 700 1$aHERVIEU-LEGER,$bDaniele$0405738 702 1$aPASQUALI,$bAldo 801 0$aIT$bsalbc$gISBD 912 $a990000707550203316 951 $aII.2. 88(VARIE COLL. 23/448)$b129330 LM$cVARIE COLL. 951 $aII.2. 88b(VARIE COLL. 23/448 BIS)$b136907 LM$cVARIE COLL. 951 $aII.2. 88a(VARIE COLL. 23/448 A)$b136908 LM$cVARIE COLL. 959 $aBK 969 $aUMA 979 $aPATTY$b90$c20011025$lUSA01$h1313 979 $c20020403$lUSA01$h1719 979 $aPATRY$b90$c20040406$lUSA01$h1649 979 $aCOPAT3$b90$c20041228$lUSA01$h1137 996 $aLa religion pour mémoire$936567 997 $aUNISA LEADER 00844nam a2200229 i 4500 001 991000311939707536 005 20020506125101.0 008 981218s1970 gr ||| | gre 035 $ab10682818-39ule_inst 035 $aEXGIL143324$9ExL 040 $aBiblioteca Interfacoltà$bita 100 1 $aParlabantzas, Takes B.$0533820 245 12$aE technike tou bitraig /$cTake B. Parlabantza 260 $aAthenai :$bEthnikos Organismos hellenikos cheirotechnias,$c1970 300 $a170 p. :$bill. ;$c21 cm. 650 4$aArte vetraria 907 $a.b10682818$b02-04-14$c28-06-02 912 $a991000311939707536 945 $aLE002 Ar. I D 22$g1$i2002000975492$lle002$o-$pE0.00$q-$rl$s- $t0$u0$v0$w0$x0$y.i10776539$z28-06-02 996 $aTechnike tou bitraig$9910142 997 $aUNISALENTO 998 $ale002$b01-01-98$cm$da $e-$fgre$ggr $h2$i1 LEADER 01840oam 2200493I 450 001 9910714050603321 005 20201113125601.0 035 $a(CKB)5470000002507140 035 $a(OCoLC)761487580 035 $a(EXLCZ)995470000002507140 100 $a20111115j196810 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aFlow-field properties near an arrow-wing--body model at Mach numbers of 1.60, 2.36, and 2.96 /$fby Robert L. Weirich and Walter A. Vahl 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dOctober 1968. 215 $a1 online resource (135 pages) $cillustrations 225 1 $aNASA technical note ;$vTN D-4809 300 $a"October 1968." 320 $aIncludes bibliographical references (page 12). 606 $aSupersonic wind tunnels$xTesting 606 $aSupersonic planes$xDesign and construction 606 $aSupersonic planes$xTesting 606 $aSupersonic planes$xDesign and construction$2fast 606 $aSupersonic wind tunnels$xTesting$2fast 615 0$aSupersonic wind tunnels$xTesting. 615 0$aSupersonic planes$xDesign and construction. 615 0$aSupersonic planes$xTesting. 615 7$aSupersonic planes$xDesign and construction. 615 7$aSupersonic wind tunnels$xTesting. 700 $aWeirich$b Robert L.$01398246 702 $aVahl$b Walter A. 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910714050603321 996 $aFlow-field properties near an arrow-wing--body model at Mach numbers of 1.60, 2.36, and 2.96$93461227 997 $aUNINA