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035   $a(CKB)5470000002529284
035   $a(OCoLC)1158388810
035   $a(EXLCZ)995470000002529284
100   $a20200615d1941      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCompression tests of some 17S-T aluminum-alloy specimens of I cross section /$fby H.N. Hill
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1941.
215   $a1 online resource (12 pages, 9 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vno. 798
300   $a"March 1941."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 12).
606   $aAluminum alloys
606   $aMaterials$xCompression testing
606   $aAluminum alloys$2fast
606   $aMaterials$xCompression testing$2fast
615  0$aAluminum alloys.
615  0$aMaterials$xCompression testing.
615  7$aAluminum alloys.
615  7$aMaterials$xCompression testing.
700   $aHill$b H. N.$01391511
712 02$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   $a9910717293803321
996   $aCompression tests of some 17S-T aluminum-alloy specimens of I cross section$93512348
997   $aUNINA