02072oam 2200577 450 991071602460332120210527121304.0(CKB)5470000002517862(OCoLC)1150919719(EXLCZ)99547000000251786220200416d1936 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierA comparison of corrosion-resistant steel (18 percent chromium - 8 percent nickel) and aluminum alloy (24ST) /by J.E. SullivanWashington, [D.C.] :National Advisory Committee for Aeronautics,1936.1 online resource (12 pages)Technical note / National Advisory Committee for Aeronautics ;No. 560"March 1936."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 12).Comparison of corrosion-resistant steel AirplanesDesign and constructionAluminum alloysSteel alloysCorrosion resistant alloysAirplanesDesign and constructionfastAluminum alloysfastCorrosion resistant alloysfastSteel alloysfastAirplanesDesign and construction.Aluminum alloys.Steel alloys.Corrosion resistant alloys.AirplanesDesign and construction.Aluminum alloys.Corrosion resistant alloys.Steel alloys.Sullivan J. E.1412504United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716024603321A comparison of corrosion-resistant steel (18 percent chromium - 8 percent nickel) and aluminum alloy (24ST)3506208UNINA