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Coupling damage-sensing particles to the digitial twin concept / / Jacob D. Hochhalter [and eight others]
| Coupling damage-sensing particles to the digitial twin concept / / Jacob D. Hochhalter [and eight others] |
| Autore | Hochhalter Jacob D. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2014 |
| Descrizione fisica | 1 online resource (10 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aerospace vehicles
Cracks Shape memory alloys Crack propagation Phase transformations Maintenance Inspection |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702505903321 |
Hochhalter Jacob D.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Strain-based damage determination using finite element analysis for structural health management / / Jacob D. Hochhalter and Thiagaraja Krishnamurthy, Miguel A. Aguilo
| Strain-based damage determination using finite element analysis for structural health management / / Jacob D. Hochhalter and Thiagaraja Krishnamurthy, Miguel A. Aguilo |
| Autore | Hochhalter Jacob D. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2016 |
| Descrizione fisica | 1 online resource (14 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Damage assessment
Fatigue (materials) Finite element method Strain measurement Structural analysis Structural health monitoring |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707968203321 |
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Hochhalter Jacob D.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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