02144oam 2200565 450 991071522890332120210128141747.0(CKB)5470000002509737(OCoLC)1143006546(EXLCZ)99547000000250973720200304d1933 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierComparison of three methods for calculating the compressive strength of flat and slightly curved sheet and stiffener combinations /by Eugene E. LundquistWashington, [D.C.] :National Advisory Committee for Aeronautics,1933.1 online resource (19 pages, 12 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 455"March, 1933."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 17).AirplanesDesign and constructionMonocoque constructionPlates (Engineering)Strength of materialsAirplanesDesign and constructionfastMonocoque constructionfastPlates (Engineering)fastStrength of materialsfastAirplanesDesign and construction.Monocoque construction.Plates (Engineering)Strength of materials.AirplanesDesign and construction.Monocoque construction.Plates (Engineering)Strength of materials.Lundquist Eugene E.1386894United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910715228903321Comparison of three methods for calculating the compressive strength of flat and slightly curved sheet and stiffener combinations3541385UNINA