01796oam 2200517 450 991071716700332120220210083912.0(CKB)5470000002528545(OCoLC)1154792555(EXLCZ)99547000000252854520200519d1939 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierA method of estimating the critical buckling load for structural members /by Eugene E. LundquistWashington, [D.C.] :National Advisory Committee for Aeronautics,1939.1 online resource (25 pages, 11 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 717"July 1939."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 25).Structural designBuckling (Mechanics)Mathematical analysisBuckling (Mechanics)fastMathematical analysisfastStructural designfastStructural design.Buckling (Mechanics)Mathematical analysis.Buckling (Mechanics)Mathematical analysis.Structural design.Lundquist Eugene E.1386894United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910717167003321A method of estimating the critical buckling load for structural members3475833UNINA