LEADER 00951nam0-2200337---450- 001 990008203830403321 005 20051012122044.0 010 $a1-84169-411-8 035 $a000820383 035 $aFED01000820383 035 $a(Aleph)000820383FED01 035 $a000820383 100 $a20051012d2005----km-y0itay50------ba 101 0 $aeng 102 $aUS 105 $aa---a---101yy 200 1 $aHandbook of mathematical cognition$fJ.I.D.Campbell, editor 210 $aNew York$cPsychology press$dc2005 215 $axvii,508 p.$d24 cm 610 0 $aEducazione matematica$aCongressi 610 0 $aMatematica$aInsegnamento$aCongressi 676 $a510.71$v21 701 1$aCampbell,$bJamie I.D.$0291708 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990008203830403321 952 $aCPDM-97-055$b21171$fMA1 959 $aMA1 962 $a97-06 996 $aHandbook of mathematical cognition$9740060 997 $aUNINA LEADER 01696oam 2200517 450 001 9910716726503321 005 20210827142703.0 035 $a(CKB)5470000002524913 035 $a(OCoLC)1159597628 035 $a(EXLCZ)995470000002524913 100 $a20200623d1937 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aStability of structural members under axial load /$fby Eugene E. Lundquist 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1937. 215 $a1 online resource (29 pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 617 300 $a"October 1937." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 22). 606 $aStructural design 606 $aAxial loads 606 $aMathematical analysis 606 $aAxial loads$2fast 606 $aMathematical analysis$2fast 606 $aStructural design$2fast 615 0$aStructural design. 615 0$aAxial loads. 615 0$aMathematical analysis. 615 7$aAxial loads. 615 7$aMathematical analysis. 615 7$aStructural design. 700 $aLundquist$b Eugene E.$01386894 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910716726503321 996 $aStability of structural members under axial load$93454209 997 $aUNINA