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Aeroelastic tailoring via tow steered composites / / Bret K. Stanford, Christine V. Jutte
| Aeroelastic tailoring via tow steered composites / / Bret K. Stanford, Christine V. Jutte |
| Autore | Stanford Bret K. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2014 |
| Descrizione fisica | 1 online resource (25 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aeroelasticity
Laminates Stiffness matrix Transverse loads High aspect ratio Aerodynamic loads |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702734303321 |
Stanford Bret K.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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AF-Shell 1.0 user guide / / Mark W. McElroy
| AF-Shell 1.0 user guide / / Mark W. McElroy |
| Autore | McElroy Mark W. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2017 |
| Descrizione fisica | 1 online resource (30 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Composite materials
Computer programs Computerized simulation Impact damage Laminates |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706250103321 |
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McElroy Mark W.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Analysis methods for progressive damage of composite structures / / Cheryl A. Rose, Carlos G. Dávila, and Frank A. Leone
| Analysis methods for progressive damage of composite structures / / Cheryl A. Rose, Carlos G. Dávila, and Frank A. Leone |
| Autore | Rose Cheryl A. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2013 |
| Descrizione fisica | 1 online resource (41 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aircraft structures
Composite structures Continuums Damage assessment Laminates Structural analysis |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705295103321 |
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Rose Cheryl A.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates [[electronic resource] /] / Alexander Tessler ... [and others]
| Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates [[electronic resource] /] / Alexander Tessler ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] |
| Descrizione fisica | 1 online resource (19 pages) : illustrations |
| Altri autori (Persone) | TesslerAlexander |
| Collana | NASA/TP |
| Soggetto topico |
Composite structures
Laminates Sandwich structures Shear stress Computational mechanics Finite element method |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702003703321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders / / Michael P. Nemeth
| An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders / / Michael P. Nemeth |
| Autore | Nemeth Michael P. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013 |
| Descrizione fisica | 1 online resource (60 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Anisotropy
Axial compression loads Cylindrical shells Inhomogeneity Laminates Sandwich structures |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704816303321 |
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Nemeth Michael P.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Autoclave processing for composite material fabrication. 1. An analysis of resin flows and fiber compactions for thin laminate [[electronic resource] /] / T.H. Hou
| Autoclave processing for composite material fabrication. 1. An analysis of resin flows and fiber compactions for thin laminate [[electronic resource] /] / T.H. Hou |
| Autore | Hou T. H |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1985] |
| Descrizione fisica | 1 online resource (v, 34 pages) : digital, PDF file |
| Collana | NASA contractor report |
| Soggetto topico |
Aerospace engineering
Autoclaving Composite materials Fabrication Flow distribution Heat transfer coefficients Laminates Pressure gradients Resins Thermosetting resins Time dependence |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697170403321 |
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Hou T. H
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1985] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Combining through-thickness reinforcement and self-healing for improved damage tolerance and durability of composites / / T. Kevin O'Brien [and seven others]
| Combining through-thickness reinforcement and self-healing for improved damage tolerance and durability of composites / / T. Kevin O'Brien [and seven others] |
| Autore | O'Brien T. Kevin |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013 |
| Descrizione fisica | 1 online resource (27 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Tubes
Glass Laminates Fracturing Epoxy resins Thickness Hardeners Panels Carbon Pins |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704630403321 |
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O'Brien T. Kevin
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 |
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Hodge A. J
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| [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Composite sandwich structure and method for making same [[electronic resource] /] / inventor, Charles J. Magurany
| Composite sandwich structure and method for making same [[electronic resource] /] / inventor, Charles J. Magurany |
| Edizione | [[Redacted ed.]] |
| Pubbl/distr/stampa | [Washington, DC] : , : [National Aeronautics and Space Administration], , [1995] |
| Descrizione fisica | 1 online resource : illustrations |
| Altri autori (Persone) | MaguranyCharles J |
| Collana | NASA case |
| Soggetto topico |
Composite structures
Fabrication Laminates Ribs (supports) Sandwich structures Composite construction |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697270703321 |
| [Washington, DC] : , : [National Aeronautics and Space Administration], , [1995] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Computational implementation of a thermodynamically based work potential model for progressive microdamage and transverse cracking in fiber-reinforced laminates [[electronic resource] /] / Evan J. Pineda ... [and others]
| Computational implementation of a thermodynamically based work potential model for progressive microdamage and transverse cracking in fiber-reinforced laminates [[electronic resource] /] / Evan J. Pineda ... [and others] |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (22 pages) : color illustrations |
| Altri autori (Persone) | PinedaEvan J |
| Collana | NASA/TM |
| Soggetto topico |
Fiber composites
Laminates Continuums Failure analysis Microcracks Potential theory Transverse loads |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | und |
| Record Nr. | UNINA-9910702121403321 |
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Laminates
(49)
- Composite structures (10)
- Composite materials (9)
- Delaminating (7)
- Fiber composites (7)