LEADER 01124nam0-2200361 --450 001 9910290258703321 005 20181107135337.0 010 $a978-88-6708-443-2 100 $a20181107d2016----kmuy0itay5050 ba 101 1 $aita$cfre 102 $aIT 105 $a 001yy 200 1 $a<>declino della cristianità sotto l'islam$edal Jihad alla dhimmitudine$fBat Ye'or$g[prefazione di Jacques Ellul] 205 $a2. ed. 210 $aTorino$cLindau$d2016 215 $a563 p.$cill.$d24 cm 225 1 $a<>leoni 300 $aTraduzione dal francese di Lucilla Congiu 300 $aNome del prefatore in copertina 610 0 $aCristianesimo e islamismo 610 0 $aGuerra$aConcezione islamica 610 0 $aFondamentalismo islamico$aStoria 676 $a297.2$v19$zita 700 0$aBat Ye'or$0628922 702 1$aEllul,$bJacques 702 1$aCongiu,$bLucilla 801 0$aIT$bUNINA$gREICAT$2UNIMARC 901 $aBK 912 $a9910290258703321 952 $aXIV L 116$b2093/2018$fFSPBC 959 $aFSPBC 996 $aDeclino della cristianità sotto l'islam$91537345 997 $aUNINA LEADER 01059nam a2200277 i 4500 001 991000461549707536 005 20020503181147.0 008 010319s1988 it ||| | fre 020 $c23600 035 $ab10080892-39ule_inst 035 $aLE02516490$9ExL 040 $aFac. Economia$bita 082 0 $a448.0024651 100 1 $aCapello, F.$0460472 245 10$aCourrier contacts :$bcours de francais commercial /$cF. Capello, P. Dallera 260 $aMilano :$bGhisetti e Corvi,$cc1988 300 $a576 p. ;$c26 cm. 650 4$aLingua francese - Manuali di corrispondenza commerciale 700 1 $aDallera, P. 907 $a.b10080892$b21-09-06$c27-06-02 912 $a991000461549707536 945 $aLE025 ECO 448 CAP01.01$g1$i2025000073609$lle025$o-$pE0.00$q-$rl$s- $t0$u1$v0$w1$x0$y.i10092183$z27-06-02 945 $aLE025 ECO 448 CAP01.01$g2$i2025000073616$lle025$o-$pE0.00$q-$rl$s- $t0$u0$v0$w0$x0$y.i10092195$z27-06-02 996 $aCourrier contacts$9195600 997 $aUNISALENTO 998 $ale025$b01-01-01$cm$da $e-$ffre$git $h0$i2 LEADER 01995nam 2200565I 450 001 9910705871503321 005 20170725075709.0 035 $a(CKB)5470000002453700 035 $a(OCoLC)994642614 035 $a(EXLCZ)995470000002453700 100 $a20170725j199806 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 12$aA progressive damage methodology for residual strength predictions of notched composite panels /$fTimothy W. Coats and Charles E. Harris 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJune 1998. 215 $a1 online resource (43 pages) $cillustrations 225 1 $aNASA/TM ;$v1998-207646 300 $a"June 1998." 300 $a"Performing organization: NASA Langley Research Center"--Report documentation page. 320 $aIncludes bibliographical references (pages 22-24). 606 $aComposite structures$2nasat 606 $aCrack propagation$2nasat 606 $aEpoxy matrix composites$2nasat 606 $aFractography$2nasat 606 $aFracture mechanics$2nasat 606 $aFracture strength$2nasat 606 $aLaminates$2nasat 606 $aLoads (forces)$2nasat 606 $aResidual strength$2nasat 615 7$aComposite structures. 615 7$aCrack propagation. 615 7$aEpoxy matrix composites. 615 7$aFractography. 615 7$aFracture mechanics. 615 7$aFracture strength. 615 7$aLaminates. 615 7$aLoads (forces) 615 7$aResidual strength. 700 $aCoats$b Timothy W.$01397146 702 $aHarris$b Charles E.$f1950- 712 02$aLangley Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910705871503321 996 $aA progressive damage methodology for residual strength predictions of notched composite panels$93458432 997 $aUNINA