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100   $a20190503d1947      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe 1350°F stress-rupture properties of two wrought alloys and three cast alloys /$fby E.E. Reynolds, J.W. Freeman, and A.E. White
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1947.
215   $a1 online resource (23 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 1380
300   $a"November 1947."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 7).
517 3 $aOne thousand three hundred fifty degree fahrenheit stress-rupture properties of two wrought alloys and three cast alloys
606   $aAlloys$xEffect of temperature on
606   $aAlloys$xFatigue$xTesting
606   $aStrains and stresses
606   $aAlloys$xFatigue$xTesting$2fast
606   $aStrains and stresses$2fast
615  0$aAlloys$xEffect of temperature on.
615  0$aAlloys$xFatigue$xTesting.
615  0$aStrains and stresses.
615  7$aAlloys$xFatigue$xTesting.
615  7$aStrains and stresses.
700   $aReynolds$b E. E.$0193386
702   $aFreeman$b J. W$g(James W.),
702   $aWhite$b A. E$g(Albert Easton),$f1884-1956,
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bCOP
801  2$bTRAAL
801  2$bGPO
801  2$bSTF
801  2$bGPO
906   $aBOOK
912   $a9910713766803321
996   $aThe 1350°F stress-rupture properties of two wrought alloys and three cast alloys$93503330
997   $aUNINA