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ACT payload shroud structural concept analysis and optimization [[electronic resource] /] / Bart F. Zalewski, Brett A. Bednarcyk ; prepared for the 16th U.S. National Congress on Theoretical and Applied Mechanics (USNCTAM) sponsored by the U.S. Committee on Theoretical and Applied Mechanics, University Park, Pennsylvania, June 27-July 2, 2010
ACT payload shroud structural concept analysis and optimization [[electronic resource] /] / Bart F. Zalewski, Brett A. Bednarcyk ; prepared for the 16th U.S. National Congress on Theoretical and Applied Mechanics (USNCTAM) sponsored by the U.S. Committee on Theoretical and Applied Mechanics, University Park, Pennsylvania, June 27-July 2, 2010
Autore Zalewski Bartlomiej Francisze
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica 1 online resource (14 pages) : color illustrations
Altri autori (Persone) BednarcykBrett A
Collana NASA/TM
Soggetto topico Structural design
Fiber composites
Finite element method
Launch vehicles
Composite structures
Structural analysis
Ares 5 cargo launch vehicle
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Advanced Composites Technology payload shroud structural concept analysis and optimization
Record Nr. UNINA-9910700302703321
Zalewski Bartlomiej Francisze  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation / / W. Keats Wilkie, K.C. Park
An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation / / W. Keats Wilkie, K.C. Park
Autore Wilkie W. Keats
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1996
Descrizione fisica 1 online resource (iv, 58 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Aeroelasticity
Helicopters
Fiber composites
Rotary wings
Unsteady aerodynamics
Differential equations
Galerkin method
Numerical integration
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707239903321
Wilkie W. Keats  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Analysis of fiber clustering in composite materials using high-fidelity multiscale micromechanics / / Brett A. Bednarcyk, Jacob Aboudi, Steven M. Arnold
Analysis of fiber clustering in composite materials using high-fidelity multiscale micromechanics / / Brett A. Bednarcyk, Jacob Aboudi, Steven M. Arnold
Autore Bednarcyk Brett A.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2015
Descrizione fisica 1 online resource (30 pages) : color illustrations
Collana NASA/TM
Soggetto topico Fiber composites
Micromechanics
Microstructure
Photomicrography
Epoxy matrix composites
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910704081303321
Bednarcyk Brett A.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2015
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Annealing effects on creep and rupture of polycrystalline alumina-based fibers / / J.C. Goldsby [and three others]
Annealing effects on creep and rupture of polycrystalline alumina-based fibers / / J.C. Goldsby [and three others]
Autore Goldsby Jon C.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1998
Descrizione fisica 1 online resource (11 pages) : illustrations
Collana NASA/TM
Soggetto topico Annealing
Rupturing
Creep strength
Fiber composites
Ceramic fibers
Tensile creep
Aluminum oxides
Reinforcing fibers
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706194803321
Goldsby Jon C.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1998
Materiale a stampa
Lo trovi qui: Univ. Federico II
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An assessment of self-healing fiber reinforced composites [[electronic resource] /] / Joseph G. Smith, Jr
An assessment of self-healing fiber reinforced composites [[electronic resource] /] / Joseph G. Smith, Jr
Autore Smith Joseph G
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012]
Descrizione fisica 1 online resource (23 pages) : color illustrations
Collana NASA/TM
Soggetto topico Fiber composites
Reinforcing materials
Polymers
Mechanical properties
Epoxy resins
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702094703321
Smith Joseph G  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Buckling and vibration of fiber reinforced composite plates with nanofiber reinforced matrices [[electronic resource] /] / Christos C. Chamis and Pappu L.N. Murthy
Buckling and vibration of fiber reinforced composite plates with nanofiber reinforced matrices [[electronic resource] /] / Christos C. Chamis and Pappu L.N. Murthy
Autore Chamis C. C (Christos C.)
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Descrizione fisica 1 online resource (25 pages) : color illustrations
Altri autori (Persone) MurthyP. L. N
Collana NASA/TM
Soggetto topico Anisotropic plates
Reinforced plates
Galerkin method
Buckling
Fiber composites
Vibration
Algorithms
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701854703321
Chamis C. C (Christos C.)  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel / / David E. Myers, Evan J. Pineda [and four others]
Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel / / David E. Myers, Evan J. Pineda [and four others]
Autore Myers David E (Engineer)
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013-2014
Descrizione fisica 1 online resource (3 volumes) : color illustrations
Collana NASA/TM
Soggetto topico Fibrous composites
Finite element method
Honeycomb structures
Ares 5 cargo launch vehicle
Epoxy matrix composites
Fiber composites
Robustness (mathematics)
Sandwich structures
Soggetto genere / forma Technical reports.
Ebook
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto pt. 1. 8-ply in-autoclave facesheets -- pt. 2. 6-ply in-autoclave facesheets -- pt. 3. 8-ply out-of-autoclave facesheets.
Record Nr. UNINA-9910705251203321
Myers David E (Engineer)  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013-2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Carbon fiber strand tensile failure dynamic event characterization / / Kenneth L. Johnson, James Reeder
Carbon fiber strand tensile failure dynamic event characterization / / Kenneth L. Johnson, James Reeder
Autore Johnson Kenneth L.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2016
Descrizione fisica 1 online resource (40 pages) : color illustrations
Collana NASA/TM
Soggetto topico Carbon fibers
Composite wrapping
Failure modes
Fiber composites
Pressure vessels
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707825103321
Johnson Kenneth L.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage [[electronic resource] /] / A.J. Hodge, A.T. Nettles, and J.R. Jackson
Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage [[electronic resource] /] / A.J. Hodge, A.T. Nettles, and J.R. Jackson
Autore Hodge A. J
Pubbl/distr/stampa [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011]
Descrizione fisica 1 online resource (viii, 23 pages) : illustrations (some color)
Altri autori (Persone) NettlesA. T (Alan T.)
JacksonJ. R
Collana NASA/TP
Soggetto topico Compressive strength
Sandwich structures
Carbon fibers
Impact strength
Damage
Epoxy matrix composites
Laminates
Fiber composites
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910700760803321
Hodge A. J  
[Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
A comparison of tension and compression creep in a polymeric composite and the effects of physical aging on creep / / Thomas S. Gates, David R. Veazie, L. Catherine Brinson
A comparison of tension and compression creep in a polymeric composite and the effects of physical aging on creep / / Thomas S. Gates, David R. Veazie, L. Catherine Brinson
Autore Gates Thomas S. <1959->
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1996
Descrizione fisica 1 online resource (33 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Aging (materials)
Compression loads
Creep tests
Shear creep
Tensile tests
Compression tests
Polymer matrix composites
Fiber composites
Tension
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910690471903321
Gates Thomas S. <1959->  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

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