01779oam 2200529I 450 991071344020332120200429110746.0(CKB)5470000002501253(OCoLC)1117765914(EXLCZ)99547000000250125320190909d1923 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierTests on built-up airplane struts having initial tension in outside fibers /by T.A. Schwamb and C.S. Smith[Washington, D.C.] :National Advisory Committee for Aeronautics,1923.1 online resource (6 pages, 6 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 151"August 1923.""Abstracted by John G. Lee."No Federal Depository Library Program (FDLP) item number.AirplanesStruts (Engineering)Strains and stressesAirplanesfastStrains and stressesfastStruts (Engineering)fastAirplanes.Struts (Engineering)Strains and stresses.Airplanes.Strains and stresses.Struts (Engineering)Schwamb T. A.1415945Smith C. S.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910713440203321Tests on built-up airplane struts having initial tension in outside fibers3519571UNINA