01195nam2-2200385---450 99000567297020331620190610183131.0000567297USA01000567297(ALEPH)000567297USA0100056729720050824d1968----|||y0itaa50------baitait0 00|||<<Vol 3: Il >> problema della conoscenza nei sistemi postkantianiErnst CassirerMilanoil Saggiatore1968604 p.21 cm.0010005672922001Storia della filosofia moderna3FilosofiaStoriaSec. 13.-sec. 19.FMILANO190.9CASSIRER,Ernst45625ITSA20111219990005672970203316Dipar.to di Filosofia - SalernoDFFDC CAS SFM6417 FILXV.18.A. 182 3 (FDC CAS SFM 3)6417 FILBKFDECI20121027USA01152620121027USA011615PATRY9020130312USA011705Problema della conoscenza nei sistemi postkantiani147050UNISASA001480002881oam 2200853 450 991070525120332120210820074229.0(CKB)5470000002448855(OCoLC)889078029(EXLCZ)99547000000244885520140825g20132014 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierBuckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel /David E. Myers, Evan J. Pineda [and four others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,2013-2014.1 online resource (3 volumes) color illustrationsNASA/TM ;2013-217822NASA/TM ;2014-217822Includes bibliographical references.pt. 1. 8-ply in-autoclave facesheets -- pt. 2. 6-ply in-autoclave facesheets -- pt. 3. 8-ply out-of-autoclave facesheets.Fibrous compositesFinite element methodHoneycomb structuresFibrous compositesfastFinite element methodfastHoneycomb structuresfastAres 5 cargo launch vehiclenasatEpoxy matrix compositesnasatFiber compositesnasatFinite element methodnasatHoneycomb structuresnasatRobustness (mathematics)nasatSandwich structuresnasatTechnical reports.fastEbook.Technical reports.lcgftFibrous composites.Finite element method.Honeycomb structures.Fibrous composites.Finite element method.Honeycomb structures.Ares 5 cargo launch vehicle.Epoxy matrix composites.Fiber composites.Finite element method.Honeycomb structures.Robustness (mathematics)Sandwich structures.Myers David E(Engineer),328638Pineda Evan J.NASA Glenn Research Center,United States.National Aeronautics and Space Administration,GPOGPOGPODIBIBLWAOCLCOOCLCFINTOCLCQOCLCOXFFOCLOCLCQGPOBOOK9910705251203321Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel3539258UNINA