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001 9910709690303321
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035   $a(OCoLC)227765830
035   $a(EXLCZ)995470000002471329
100   $a20100322j199012    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAxial-torsional fatigue: a study of tubular specimen thickness effects /$fPeter J. Bonacuse and Sreeramesh Kalluri
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration,$dDecember 1990.
215   $a1 online resource (16 pages) $cillustrations
300   $a"December 1990."
300   $a"AVSCOM TM 90-C-014."
320   $aIncludes bibliographical references (pages 6-7).
517   $aAxial-torsional fatigue
606   $aFatigue life$2nasat
606   $aFatigue tests$2nasat
606   $aMeasuring instruments$2nasat
606   $aAxial strain$2nasat
606   $aDeformation$2nasat
615  7$aFatigue life.
615  7$aFatigue tests.
615  7$aMeasuring instruments.
615  7$aAxial strain.
615  7$aDeformation.
700   $aBonacuse$b Peter J.$f1960-$01406621
702   $aKalluri$b Sreeramesh
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aUnited States.$bArmy Aviation Systems Command.
801  0$bDTICE
801  1$bDTICE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910709690303321
996   $aAxial-torsional fatigue: a study of tubular specimen thickness effects$93528466
997   $aUNINA