Info
- Utilizzare la checkbox di selezione a fianco di ciascun documento per attivare le funzionalità di stampa, invio email, download nei formati disponibili del (i) record.
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 | ||
| ||
A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications [[electronic resource] /] / A.T. Nettles
| A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications [[electronic resource] /] / A.T. Nettles |
| Autore | Nettles A. T (Alan T.) |
| Pubbl/distr/stampa | Huntsville, Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011] |
| Descrizione fisica | 1 online resource (vii, 39 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Compressive strength
Impact strength Honeycomb structures Launch vehicles Damage Tolerances (mechanics) Residual strength |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701853303321 |
|
Nettles A. T (Alan T.)
|
||
| Huntsville, Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy / / A.T. Nettles and D.G. Lance
| The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy / / A.T. Nettles and D.G. Lance |
| Autore | Nettles A. T (Alan T.) |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical, Information Program, , 1992 |
| Descrizione fisica | 1 online resource (iv, 16 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Impact strength
Epoxy matrix composites Prestressing Strain distribution Impact tests Compression loads Compressive strength |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707973403321 |
|
Nettles A. T (Alan T.)
|
||
| [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical, Information Program, , 1992 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Elevated temperature compressive strength properties of oxide dispersion strengthened NiAl after cryomilling and roasting in nitrogen / / J. Daniel Whittenberger [and others]
| Elevated temperature compressive strength properties of oxide dispersion strengthened NiAl after cryomilling and roasting in nitrogen / / J. Daniel Whittenberger [and others] |
| Autore | Whittenberger J. Daniel (John Daniel) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1998 |
| Descrizione fisica | 1 online resource (31 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Intermetallics
Aluminum nitrides Nickel aluminides Milling (machining) Mechanical properties Roasting Oxide dispersion strengthening Compressive strength |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705862303321 |
|
Whittenberger J. Daniel (John Daniel)
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1998 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Evaluation of the behavior of Technova Corporation rod-stiffened stitched compression specimens / / Dawn C. Jegley
| Evaluation of the behavior of Technova Corporation rod-stiffened stitched compression specimens / / Dawn C. Jegley |
| Autore | Dawn C. Jegley |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013 |
| Descrizione fisica | 1 online resource (21 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Axial stress
Compression loads Compressive strength Epoxy matrix composites Pultrusion |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702419603321 |
|
Dawn C. Jegley
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Hot/wet open hole compression strength of carbon/epoxy laminates for launch vehicle applications [[electronic resource] /] / A.T. Nettles
| Hot/wet open hole compression strength of carbon/epoxy laminates for launch vehicle applications [[electronic resource] /] / A.T. Nettles |
| Autore | Nettles A. T (Alan T.) |
| Pubbl/distr/stampa | [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2009] |
| Descrizione fisica | 1 online resource (vii, 23 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Epoxy matrix composites
Temperature effects Compressive strength Launch vehicles Safety factors |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910700382303321 |
|
Nettles A. T (Alan T.)
|
||
| [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2009] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Modeling fiber kinking at the microscale and mesoscale / / Miguel Herraʹez [and three others]
| Modeling fiber kinking at the microscale and mesoscale / / Miguel Herraʹez [and three others] |
| Autore | Herráez Miguel |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2018 |
| Descrizione fisica | 1 online resource (80 pages) : illustrations (mostly color) |
| Collana | NASA/TP |
| Soggetto topico |
Kinking
Micromechanics Fiber orientation Mesoscale phenomena Compressive strength |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910711660003321 |
|
Herráez Miguel
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2018 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Notched strength allowables and inplane shear strength of AS4/VRM-34 textile laminates / / Ray W. Grenoble, William M. Johnston
| Notched strength allowables and inplane shear strength of AS4/VRM-34 textile laminates / / Ray W. Grenoble, William M. Johnston |
| Autore | Grenoble Ray W. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2013 |
| Descrizione fisica | 1 online resource (21 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Carbon fibers
Compressive strength Epoxy resins Fiber composites Mathematical models Notch tests Shear strength |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702429203321 |
|
Grenoble Ray W.
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Probabilistic simulation for combined cycle fatigue in composites [[electronic resource] /] / Christos C. Chamis
| Probabilistic simulation for combined cycle fatigue in composites [[electronic resource] /] / Christos C. Chamis |
| Autore | Chamis C. C (Christos C.) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (13 pages) : illustrations |
| Collana | NASA TM- |
| Soggetto topico |
Aging (materials)
Compressive strength Graphite-epoxy composites Fracture strength Polymer matrix composites Thermal fatigue Probability theory Failure modes Fatigue life |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699505703321 |
|
Chamis C. C (Christos C.)
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Probabilistic simulation for combined thermo-mechanical cyclic fatigue in composites [[electronic resource] /] / Christos C. Chamis
| Probabilistic simulation for combined thermo-mechanical cyclic fatigue in composites [[electronic resource] /] / Christos C. Chamis |
| 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 (13 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Graphite-epoxy composites
Fatigue life Time temperature parameter Thermodynamics Thermal fatigue Matrix materials Laminates Compressive strength Aging (materials) Polymer matrix composites Temperature dependence |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701468703321 |
|
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 | ||
| ||
