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100   $a20120408j196901    ua             0
101 0 $aeng
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
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200 10$aTensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ?to 400 ?F (370 ?to 480 ?K) /$fby Dick M. Royster
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dJanuary 1969.
215   $a1 online resource (42 pages) $cillustrations
225 1 $aNASA/TN ;$vD-5010
300   $a"January 1969."
320   $aIncludes bibliographical references (page 12).
517   $aTensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ?to 400 ?F 
606   $aTensile properties$2nasat
606   $aAluminum alloys$xDuctility
606   $aAluminum alloys$xCreep
606   $aSupersonic transport planes$xMaterials$xEnvironmental testing
606   $aAluminum alloys$xCreep$2fast
606   $aAluminum alloys$xDuctility$2fast
615  7$aTensile properties.
615  0$aAluminum alloys$xDuctility.
615  0$aAluminum alloys$xCreep.
615  0$aSupersonic transport planes$xMaterials$xEnvironmental testing.
615  7$aAluminum alloys$xCreep.
615  7$aAluminum alloys$xDuctility.
700   $aRoyster$b Dick M.$01399411
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
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906   $aBOOK
912   $a9910716061303321
996   $aTensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ?to 400 ?F (370 ?to 480 ?K)$93486920
997   $aUNINA