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The impact response of carbon/epoxy laminates / / A.T. Nettles and A.J. Hodge
The impact response of carbon/epoxy laminates / / A.T. Nettles and A.J. Hodge
Autore Nettles A. T (Alan T.)
Pubbl/distr/stampa Marshall Space Flight Center, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , November 1997
Descrizione fisica 1 online resource (viii, 165 pages) : illustrations
Collana NASA/TM
Soggetto topico Epoxy matrix composites
Laminates
Impact tests
Dynamic tests
Soggetto genere / forma Technical Memorandum
Soggetto non controllato Impact Phenomena
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705766303321
Nettles A. T (Alan T.)  
Marshall Space Flight Center, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , November 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Mechanical properties of graphene nanoplatelet/carbon fiber/epoxy hybrid composites : multiscale modeling and experiments / / C.M. Hadden [and seven others]
Mechanical properties of graphene nanoplatelet/carbon fiber/epoxy hybrid composites : multiscale modeling and experiments / / C.M. Hadden [and seven others]
Autore Hadden C. M.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2015
Descrizione fisica 1 online resource (20 pages) : color illustrations
Collana NASA/TM
Soggetto topico Nanocomposites
Epoxy matrix composites
Micromechanics
Graphene
Carbon fibers
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Mechanical properties of graphene nanoplatelet/carbon fiber/epoxy hybrid composites
Record Nr. UNINA-9910704274303321
Hadden C. M.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2015
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Mode II interlaminar fracture toughness and fatigue characterization of a graphite epoxy composite material [[electronic resource] /] / T. Kevin O'Brien, William M. Johnston, Gregory J. Toland
Mode II interlaminar fracture toughness and fatigue characterization of a graphite epoxy composite material [[electronic resource] /] / T. Kevin O'Brien, William M. Johnston, Gregory J. Toland
Autore O'Brien T. Kevin
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2010]
Descrizione fisica 1 online resource (28 pages) : illustrations
Altri autori (Persone) JohnstonWilliam M
TolandGregory J
Collana NASA/TM
Soggetto topico Composite materials
Graphite-epoxy composites
Fracture mechanics
Fracture strength
Delaminating
Epoxy matrix composites
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910700152003321
O'Brien T. Kevin  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Multiscale static analysis of notched and unnotched laminates using the generalized method of cells / / Paria Naghipour Ghezeljeh [and six others]
Multiscale static analysis of notched and unnotched laminates using the generalized method of cells / / Paria Naghipour Ghezeljeh [and six others]
Autore Ghezeljeh Paria Naghipour
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2016
Descrizione fisica 1 online resource (37 pages) : color illustrations
Collana NASA/TM
Soggetto topico Composite materials
Epoxy matrix composites
Laminates
Micromechanics
Nonlinearity
Stress-strain relationships
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707427003321
Ghezeljeh Paria Naghipour  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Prediction of composite laminate fracture: micromechanics and progressive fracture / / P.K. Gotsis and C.C. Chamis, L. Minnetyan
Prediction of composite laminate fracture: micromechanics and progressive fracture / / P.K. Gotsis and C.C. Chamis, L. Minnetyan
Autore Gotsis Pascal K.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1996
Descrizione fisica 1 online resource (14 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Glass fibers
Graphite-epoxy composites
Matrix materials
Laminates
Epoxy matrix composites
Residual stress
Stress-strain relationships
Graphite
Fiber composites
Composite materials
Fracture mechanics
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Prediction of composite laminate fracture
Record Nr. UNINA-9910707334103321
Gotsis Pascal K.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Progressive damage analysis of bonded composite joints / / Frank A. Leone, Jr., Donato Girolamo, Carlos G. Dávila
Progressive damage analysis of bonded composite joints / / Frank A. Leone, Jr., Donato Girolamo, Carlos G. Dávila
Autore Leone Frank A.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012
Descrizione fisica 1 online resource (iii, 39 pages) : color illustrations
Collana NASA/TM
Soggetto topico Epoxy matrix composites
Delaminating
Damage assessment
Adhesive bonding
Bonded joints
Sandwich structures
Honeycomb structures
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910704686203321
Leone Frank A.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
A progressive damage methodology for residual strength predictions of notched composite panels / / Timothy W. Coats and Charles E. Harris
A progressive damage methodology for residual strength predictions of notched composite panels / / Timothy W. Coats and Charles E. Harris
Autore Coats Timothy W.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , June 1998
Descrizione fisica 1 online resource (43 pages) : illustrations
Collana NASA/TM
Soggetto topico Composite structures
Crack propagation
Epoxy matrix composites
Fractography
Fracture mechanics
Fracture strength
Laminates
Loads (forces)
Residual strength
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705871503321
Coats Timothy W.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , June 1998
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Properties of two carbon composite materials using LTM25 epoxy resin / / Juan R. Cruz, C.H. Shah and A.S. Postyn
Properties of two carbon composite materials using LTM25 epoxy resin / / Juan R. Cruz, C.H. Shah and A.S. Postyn
Autore Cross John R.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1996
Descrizione fisica 1 online resource (24 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Epoxy resins
Carbon fibers
Curing
Composite structures
Environmental tests
Epoxy matrix composites
Prepregs
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707912803321
Cross John R.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
A test for characterizing delamination migration in carbon/epoxy tape laminates / / James G. Ratcliffe, Michael W. Czabaj and Thomas K. O'Brien
A test for characterizing delamination migration in carbon/epoxy tape laminates / / James G. Ratcliffe, Michael W. Czabaj and Thomas K. O'Brien
Autore Ratcliffe James G.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2013
Descrizione fisica 1 online resource (19 pages) : color illustrations
Collana NASA/TM
Soggetto topico Cantilever beams
Delaminating
Epoxy matrix composites
Fractography
Kinking
Finite element method
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Test for characterizing delamination migration in carbon epoxy tape laminates
Record Nr. UNINA-9910705295503321
Ratcliffe James G.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

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