01349oam 2200409 450 991071519720332120201204150040.0(CKB)5470000002508037(OCoLC)761321284(EXLCZ)99547000000250803720111115j196808 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierPrediction of fatigue-crack-propagation behavior in panels with simulated rivet forces /by I.E. Figge and J.C. Newman, Jr1 online resource (32 pages) illustrationsNASA technical note ;TN D-4702"August 1968."Includes bibliographical references (pages 16-17).Aluminum alloysFatigueAnalysisAluminum alloysFatigueAnalysis.Figge I. E.1402915Newman J. C.United States.National Aeronautics and Space Administration,Langley Research Center.OCLCEOCLCEOCLCQOCLCOOCLCQGPOBOOK9910715197203321Prediction of fatigue-crack-propagation behavior in panels with simulated rivet forces3474419UNINA