LEADER 01727oam 2200517 450 001 9910716035503321 005 20210521132237.0 035 $a(CKB)5470000002517752 035 $a(OCoLC)1150919532 035 $a(EXLCZ)995470000002517752 100 $a20200416d1935 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 14$aThe initial torsional stiffness of shells with interior webs /$fby Paul Kuhn 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1935. 215 $a1 online resource (15 pages, 9 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 542 300 $a"September 1935." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (pages 13-14). 606 $aStrains and stresses 606 $aAirframes 606 $aAeronautics$xResearch 606 $aAeronautics$xResearch$2fast 606 $aAirframes$2fast 606 $aStrains and stresses$2fast 615 0$aStrains and stresses. 615 0$aAirframes. 615 0$aAeronautics$xResearch. 615 7$aAeronautics$xResearch. 615 7$aAirframes. 615 7$aStrains and stresses. 700 $aKuhn$b Paul$03498 712 02$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 $a9910716035503321 996 $aThe initial torsional stiffness of shells with interior webs$93464882 997 $aUNINA