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100   $a20200416d1936      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA comparison of corrosion-resistant steel (18 percent chromium - 8 percent nickel) and aluminum alloy (24ST) /$fby J.E. Sullivan
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1936.
215   $a1 online resource (12 pages)
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 560
300   $a"March 1936."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 12).
517   $aComparison of corrosion-resistant steel 
606   $aAirplanes$xDesign and construction
606   $aAluminum alloys
606   $aSteel alloys
606   $aCorrosion resistant alloys
606   $aAirplanes$xDesign and construction$2fast
606   $aAluminum alloys$2fast
606   $aCorrosion resistant alloys$2fast
606   $aSteel alloys$2fast
615  0$aAirplanes$xDesign and construction.
615  0$aAluminum alloys.
615  0$aSteel alloys.
615  0$aCorrosion resistant alloys.
615  7$aAirplanes$xDesign and construction.
615  7$aAluminum alloys.
615  7$aCorrosion resistant alloys.
615  7$aSteel alloys.
700   $aSullivan$b J. E.$01412504
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910716024603321
996   $aA comparison of corrosion-resistant steel (18 percent chromium - 8 percent nickel) and aluminum alloy (24ST)$93506208
997   $aUNINA