LEADER 01797nam  2200529   450 
001 9910706554003321
005 20171129131529.0
035   $a(CKB)5470000002456907
035   $a(OCoLC)1013466540
035   $a(EXLCZ)995470000002456907
100   $a20171129j200104    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aHigh temperature fatigue crack growth behavior of Alloy 10 /$fJohn Gayda
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dApril 2001.
215   $a1 online resource (14 pages) $cillustrations
225 1 $aNASA/TM ;$v2001-210814
300   $a"April 2001."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
320   $aIncludes bibliographical references (page 4).
606   $aCrack propagation$2nasat
606   $aEngine design$2nasat
606   $aFracture strength$2nasat
606   $aHeat of solution$2nasat
606   $aHigh strength alloys$2nasat
606   $aNiobium$2nasat
606   $aTantalum$2nasat
606   $aThermal fatigue$2nasat
615  7$aCrack propagation.
615  7$aEngine design.
615  7$aFracture strength.
615  7$aHeat of solution.
615  7$aHigh strength alloys.
615  7$aNiobium.
615  7$aTantalum.
615  7$aThermal fatigue.
700   $aGayda$b John$01400320
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706554003321
996   $aHigh temperature fatigue crack growth behavior of Alloy 10$93476733
997   $aUNINA