LEADER 01845oam 2200517 450 001 9910716036103321 005 20210521115528.0 035 $a(CKB)5470000002517746 035 $a(OCoLC)1150919530 035 $a(EXLCZ)995470000002517746 100 $a20200416d1935 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 12$aA deflection formula for single-span beams of constant section subjected to combined axial and transverse loads /$fby Walter E. Burke 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1935. 215 $a1 online resource (24 pages, 21 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 540 300 $a"September 1935." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 16). 606 $aAxial loads 606 $aAirplanes$xFuselage 606 $aAeronautics$xResearch 606 $aAeronautics$xResearch$2fast 606 $aAirplanes$xFuselage$2fast 606 $aAxial loads$2fast 615 0$aAxial loads. 615 0$aAirplanes$xFuselage. 615 0$aAeronautics$xResearch. 615 7$aAeronautics$xResearch. 615 7$aAirplanes$xFuselage. 615 7$aAxial loads. 700 $aBurke$b Walter E.$01399821 712 02$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 $a9910716036103321 996 $aA deflection formula for single-span beams of constant section subjected to combined axial and transverse loads$93465776 997 $aUNINA