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100   $a20081119d1988      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $ch$2rdamedia
183   $ahe$2rdacarrier
200 10$aCharacterization of fatigue crack initiation and propagation in Ti-6Al-4V with electrical potential drop technique$b[microform] /$fSreeramesh Kalluri and Jack Telesman
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration,$d[1988]
215   $a1 volume
225 1 $aNASA technical memorandum ;$v100877
606   $aCrack initiation$2nasat
606   $aCrack propagation$2nasat
606   $aDamage assessment$2nasat
606   $aElectric potential$2nasat
606   $aMetal fatigue$2nasat
615  7$aCrack initiation.
615  7$aCrack propagation.
615  7$aDamage assessment.
615  7$aElectric potential.
615  7$aMetal fatigue.
700   $aKalluri$b Sreeramesh$01410253
701   $aTelesman$b Jack$01398014
712 02$aUnited States.$bNational Aeronautics and Space Administration.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910697714903321
996   $aCharacterization of fatigue crack initiation and propagation in Ti-6Al-4V with electrical potential drop technique$93544676
997   $aUNINA