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Development and application of benchmark examples for mixed-mode I/II quasi-static delamination propagation predictions / / Ronald Krueger
| Development and application of benchmark examples for mixed-mode I/II quasi-static delamination propagation predictions / / Ronald Krueger |
| Autore | Krueger Ronald |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2012 |
| Descrizione fisica | 1 online resource (57 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Delaminating
Finite element method Loads (forces) Crack closure Cantilever beams |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702005103321 |
Krueger Ronald
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Development and application of benchmark examples for mode II static delamination propagation and fatigue growth predictions [[electronic resource] /] / Ronald Krueger
| Development and application of benchmark examples for mode II static delamination propagation and fatigue growth predictions [[electronic resource] /] / Ronald Krueger |
| Autore | Krueger Ronald |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center : , : National Institute of Aerospace, , [2011] |
| Descrizione fisica | 1 online resource (68 pages) : color illustrations |
| Collana | [NASA contractor report] |
| Soggetto topico |
Delaminating
Mathematical models Fatigue (materials) Flexing Crack closure Stress propagation Static loads |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701781203321 |
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Krueger Ronald
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center : , : National Institute of Aerospace, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An enriched shell finite element for progressive damage simulation in composite laminates / / Mark W. McElroy
| An enriched shell finite element for progressive damage simulation in composite laminates / / Mark W. McElroy |
| Autore | McElroy Mark W. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , June 2016 |
| Descrizione fisica | 1 online resource (53 pages) : color illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Composite materials
Composite structures Crack closure Delaminating Laminates |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705740703321 |
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McElroy Mark W.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , June 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Fatigue resistance of liquid-assisted self-repairing aluminum alloys reinforced with shape memory alloys : Shape Memory Alloy Self-Healing (SMASH) technology for aeronautical applications / / M. Clara Wright, Dr. Michele Manuel, Dr. Terryl Wallace
| Fatigue resistance of liquid-assisted self-repairing aluminum alloys reinforced with shape memory alloys : Shape Memory Alloy Self-Healing (SMASH) technology for aeronautical applications / / M. Clara Wright, Dr. Michele Manuel, Dr. Terryl Wallace |
| Autore | Wright M. Clara |
| Pubbl/distr/stampa | [Cocoa Beach, FL] : , : [NASA Kennedy Space Center], , September 2013 |
| Descrizione fisica | 1 online resource (18 unnumbered pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aluminum alloys
Fatigue (materials) Shape memory alloys Crack closure Fracture strength Technology utilization |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Fatigue resistance of liquid-assisted self-repairing aluminum alloys reinforced with shape memory alloys |
| Record Nr. | UNINA-9910703411103321 |
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Wright M. Clara
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| [Cocoa Beach, FL] : , : [NASA Kennedy Space Center], , September 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Fatigue-life prediction methodology using small-crack theory / / J.C. Newman, Jr. and E.P. Phillips, M.H. Swain
| Fatigue-life prediction methodology using small-crack theory / / J.C. Newman, Jr. and E.P. Phillips, M.H. Swain |
| Autore | Newman J. C. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , January 1997 |
| Descrizione fisica | 1 online resource (29 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Crack closure
Fatigue life Crack propagation Plastic properties Stress intensity factors Models Crack tips |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707905103321 |
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Newman J. C.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , January 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Floating node method and virtual crack closure techique for modeling matrix cracking-delamination interaction / / N.V. De Carvalho [and five others]
| Floating node method and virtual crack closure techique for modeling matrix cracking-delamination interaction / / N.V. De Carvalho [and five others] |
| Autore | De Carvalho N. V. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2013 |
| Descrizione fisica | 1 online resource (17 pages) : color illustrations |
| Collana | NASA-CR |
| Soggetto topico |
Crack closure
Fracture mechanics Delaminating Ply orientation Laminates |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Floating node method and virtual crack closure technique for modeling matrix cracking delamination interaction |
| Record Nr. | UNINA-9910705251603321 |
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De Carvalho N. V.
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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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Influence of finite element software on energy release rates computed using the virtual crack closure technique [[electronic resource] /] / Ronald Krueger, Dirk Goetze
| Influence of finite element software on energy release rates computed using the virtual crack closure technique [[electronic resource] /] / Ronald Krueger, Dirk Goetze |
| Autore | Krueger Ronald |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2006] |
| Descrizione fisica | 1 online resource (49 pages) : illustrations (some color) |
| Altri autori (Persone) | GoetzeDirk |
| Collana | NAS/CR |
| Soggetto topico |
Finite element method
Strain energy release rate Crack closure Delaminating |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699315103321 |
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Krueger Ronald
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2006] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Mitigation of crack damage in metallic materials / / Patrick Leser [and seven others]
| Mitigation of crack damage in metallic materials / / Patrick Leser [and seven others] |
| Autore | Leser Patrick E. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2014 |
| Descrizione fisica | 1 online resource (17 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Fatigue (materials)
Tolerances (mechanics) Crack opening displacement Metal fatigue Crack closure Crack propagation Titanium alloys Aerospace vehicles |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702505603321 |
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Leser Patrick E.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A thermodynamically consistent damage model for advanced composites [[electronic resource] /] / Pere Maimí ... [and others]
| A thermodynamically consistent damage model for advanced composites [[electronic resource] /] / Pere Maimí ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2006] |
| Descrizione fisica | 1 online resource (42 pages) : illustrations |
| Altri autori (Persone) | MaimíPere |
| Collana | NASA/TM- |
| Soggetto topico |
Composite materials
Damage Continuum modeling Fiber composites Crack closure Degradation Loads (forces) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697164503321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2006] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Crack closure
(9)
- Delaminating (5)
- Fatigue (materials) (3)
- Composite materials (2)
- Crack propagation (2)