LEADER 01062nam2-2200361---450- 001 990003202670203316 005 20090306115824.0 010 $a3-423-05126-4 035 $a000320267 035 $aUSA01000320267 035 $a(ALEPH)000320267USA01 035 $a000320267 100 $a20090306d1971----km-y0itay50------ba 101 $ager 102 $aDE 105 $a||||||||001yy 200 1 $a<> : Italienische Reise$eDritter Teil$fJohann Wolfgang Goethe$gmit einem Nachwort von Harald Keller 210 $aMünchen$cDeutscher Taschenbuch Verlag$d1971 215 $a205 p.$d18 cm 225 2 $aDtv Gesamtausgabe$v26 410 0$12001$aDtv Gesamtausgabe 454 1$12001 461 1$1001000320191$12001 700 1$aGOETHE,$bJohann Wolfgang : von$0151776 702 1$aKELLER,$bHarald 801 0$aIT$bsalbc$gISBD 912 $a990003202670203316 951 $aII.3.A.443/26.3$b2413/26 DSLL 959 $aBK 969 $aDSLL 979 $aDSLL$b90$c20090306$lUSA01$h1158 996 $aItalienische Reise$923788 997 $aUNISA LEADER 01733oam 2200505 450 001 9910717118903321 005 20220215124216.0 035 $a(CKB)5470000002529030 035 $a(OCoLC)1157237705 035 $a(EXLCZ)995470000002529030 100 $a20200608d1940 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aChart for critical compressive stress of flat rectangular plates /$fby H.N. Hill 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics ;$d1940. 215 $a1 online resource (14 pages, 2 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vno. 773 300 $a"August 1940." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (pages 14). 606 $aPlates (Engineering) 606 $aStrains and stresses 606 $aMaterials$xCompression testing 606 $aPlates (Engineering)$2fast 606 $aStrains and stresses$2fast 615 0$aPlates (Engineering) 615 0$aStrains and stresses. 615 0$aMaterials$xCompression testing. 615 7$aPlates (Engineering) 615 7$aStrains and stresses. 700 $aHill$b H. N.$01391511 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bTRAAL 801 2$bOCLCO 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910717118903321 996 $aChart for critical compressive stress of flat rectangular plates$93445356 997 $aUNINA