02188oam 2200649I 450 991071667080332120210706130153.0(CKB)5470000002523456(OCoLC)24164755(OCoLC)762079297(OCoLC)785245209(EXLCZ)99547000000252345619910801j197304 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierA material selection method based on material properties and operating parameters /by Wolf Elber and John R. DavidsonWashington, D.C. :National Aeronautics and Space Administration,April 1973.1 online resource (12 pages) illustrationsNASA/TN ;D-7221"April 1973."Includes bibliographical references (page 8).Fracture mechanicsnasatAluminum alloysnasatFracture mechanicsMathematical modelsAluminum alloysCrackingAluminum alloysFractureAluminum alloysCrackingfastAluminum alloysFracturefastFracture mechanicsMathematical modelsfastFracture mechanics.Aluminum alloys.Fracture mechanicsMathematical models.Aluminum alloysCracking.Aluminum alloysFracture.Aluminum alloysCracking.Aluminum alloysFracture.Fracture mechanicsMathematical models.Elber Wolf1420354Davidson John R.United States.National Aeronautics and Space Administration,Langley Research Center.ABCABCAD#OCLCEOCLCQOCLCOOCLCFOCLCQOCLCOOCLCQGPOBOOK9910716670803321A material selection method based on material properties and operating parameters3537950UNINA