01831nam 2200481 450 991070704400332120160324160402.0(CKB)5470000002461049(OCoLC)945556941(EXLCZ)99547000000246104920160324j199710 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAn experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses /Edward P. PhillipsHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,October 1997.1 online resource (14 pages) illustrationsNASA technical memorandum ;4784Title from title screen (viewed March 24, 2016)."October 1997.""Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.Includes bibliographical references (page 5).Crack propagationnasatFatigue (materials)nasatAluminumnasatBending fatiguenasatAluminum alloysnasatCrack propagation.Fatigue (materials)Aluminum.Bending fatigue.Aluminum alloys.Phillips Edward P.1412274Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910707044003321An experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses3505284UNINA