02052oam 2200565 450 991071725110332120220321140656.0(CKB)5470000002529715(OCoLC)1158388807(EXLCZ)99547000000252971520200615d1941 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe effect of methods of testing on the ultimate loads supported by stiffened flat sheet panels under edge compression /by Marshall HoltWashington, [D.C.] :National Advisory Committee for Aeronautics,1941.1 online resource (19 pages, 7 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;no. 811"June 1941."No Federal Depository Library Program (FDLP) item number.Includes bibliographical reference (page 13).Aluminum alloysSheet-metalTestingMaterialsCompression testingLoads (Mechanics)Aluminum alloysfastLoads (Mechanics)fastMaterialsCompression testingfastSheet-metalTestingfastAluminum alloys.Sheet-metalTesting.MaterialsCompression testing.Loads (Mechanics)Aluminum alloys.Loads (Mechanics)MaterialsCompression testing.Sheet-metalTesting.Holt M(Marshall),1395606United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910717251103321The effect of methods of testing on the ultimate loads supported by stiffened flat sheet panels under edge compression3459740UNINA