01845oam 2200517 450 991071603610332120210521115528.0(CKB)5470000002517746(OCoLC)1150919530(EXLCZ)99547000000251774620200416d1935 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierA deflection formula for single-span beams of constant section subjected to combined axial and transverse loads /by Walter E. BurkeWashington, [D.C.] :National Advisory Committee for Aeronautics,1935.1 online resource (24 pages, 21 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 540"September 1935."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 16).Axial loadsAirplanesFuselageAeronauticsResearchAeronauticsResearchfastAirplanesFuselagefastAxial loadsfastAxial loads.AirplanesFuselage.AeronauticsResearch.AeronauticsResearch.AirplanesFuselage.Axial loads.Burke Walter E.1399821United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716036103321A deflection formula for single-span beams of constant section subjected to combined axial and transverse loads3465776UNINA