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100   $a19910801j197304    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA material selection method based on material properties and operating parameters /$fby Wolf Elber and John R. Davidson
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dApril 1973.
215   $a1 online resource (12 pages) $cillustrations
225 1 $aNASA/TN ;$vD-7221
300   $a"April 1973."
320   $aIncludes bibliographical references (page 8).
606   $aFracture mechanics$2nasat
606   $aAluminum alloys$2nasat
606   $aFracture mechanics$xMathematical models
606   $aAluminum alloys$xCracking
606   $aAluminum alloys$xFracture
606   $aAluminum alloys$xCracking$2fast
606   $aAluminum alloys$xFracture$2fast
606   $aFracture mechanics$xMathematical models$2fast
615  7$aFracture mechanics.
615  7$aAluminum alloys.
615  0$aFracture mechanics$xMathematical models.
615  0$aAluminum alloys$xCracking.
615  0$aAluminum alloys$xFracture.
615  7$aAluminum alloys$xCracking.
615  7$aAluminum alloys$xFracture.
615  7$aFracture mechanics$xMathematical models.
700   $aElber$b Wolf$01420354
702   $aDavidson$b John R.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bABC
801  1$bABC
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801  2$bGPO
906   $aBOOK
912   $a9910716670803321
996   $aA material selection method based on material properties and operating parameters$93537950
997   $aUNINA