01678oam 2200481 450 991071504320332120201120092941.0(CKB)5470000002507573(OCoLC)761147463(EXLCZ)99547000000250757320111115j196809 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEffect of residual stress on fracture strength of AISI 301 stainless-steel and Ti-5A1-2.5Sn eli titanium cracked thin-wall cylinders /by Frederick D. CalfoWashington, D.C. :National Aeronautics and Space Administration,September 1968.1 online resource (ii, 24 pages) illustrationsNASA technical note ;TN D-4777"September 1968."Includes bibliographical references (page 17).Residual stressesCylindersTestingCylindersTestingfastResidual stressesfastResidual stresses.CylindersTesting.CylindersTesting.Residual stresses.Calfo Frederick D.1416554United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCFOCLCOOCLCQGPOBOOK9910715043203321Effect of residual stress on fracture strength of AISI 301 stainless-steel and Ti-5A1-2.5Sn eli titanium cracked thin-wall cylinders3522316UNINA