01042nam--2200373---450-99000593169020331620140225093533.0000593169USA01000593169(ALEPH)000593169USA0100059316920140225d1972----km-y0itay50------balatIT||||||||001yyImperium romanumtributim discriptumJos. Wilhelm KubitschekRoma<<L'>> Erma di Bretschneider1972276 p.24 cmStudia historica121Ripr. facs. dell'ed. : Praha, 18892001Studia historica1212001001-------2001Epigrafia latinaBNCF471.1KUBITSCHEK,Jos. Wilhelm397636ITsalbcISBD990005931690203316AE 1338030 DSABKDSADSA9020140225USA010935Imperium Romanum569829UNISA01839oam 2200529I 450 991070791050332120170223142801.0(CKB)5470000002469468(OCoLC)844605483(EXLCZ)99547000000246946820130526j199702 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierDamage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets /David M. McGowan and Damodar R. AmburHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,February 1997.1 online resource (37 pages) illustrationsNASA technical memorandum ;110303"February 1997.""Performing organization: NASA Langley Research Center" Report documentation page.Includes bibliographical references (pages 12-13).Graphite-epoxy compositesnasatHoneycomb coresnasatImpact damagenasatNotch sensitivitynasatSandwich structuresnasatGraphite-epoxy composites.Honeycomb cores.Impact damage.Notch sensitivity.Sandwich structures.McGowan David M.1400479Ambur Damodar R.Langley Research Center,OCLCEOCLCEOCLCOOCLCQOCLCFOCLCQGPOBOOK9910707910503321Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets3467456UNINA