01606nam 2200445I 450 991070625030332120171018073201.0(CKB)5470000002455934(OCoLC)1006582786(EXLCZ)99547000000245593420171018j201708 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierConstitutive modeling of the facesheet to core interface in honeycomb sandwich panels subject to mode I delamination / Daniel Höwer [and five others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,August 2017.1 online resource (44 pages) color illustrationsNASA/TM ;2017-219470"August 2017."Includes bibliographical references (pages 39-44).Carbon fibersnasatDelaminatingnasatFinite element methodnasatHoneycomb structuresnasatSandwich structuresnasatCarbon fibers.Delaminating.Finite element method.Honeycomb structures.Sandwich structures.Höwer Daniel1413659NASA Glenn Research Center,GPOGPOBOOK9910706250303321Constitutive modeling of the facesheet to core interface in honeycomb sandwich panels subject to mode I delamination3510566UNINA