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Development and calibration of a system-integrated rotorcraft finite element model for impact scenarios / / Martin S. Annett [and four others]
| Development and calibration of a system-integrated rotorcraft finite element model for impact scenarios / / Martin S. Annett [and four others] |
| Autore | Annett Martin S. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012 |
| Descrizione fisica | 1 online resource (62 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Helicopters
Crashworthiness Impact loads Finite element method Calibrating Rotary wing aircraft |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704474403321 |
Annett Martin S.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Evaluation of the first transport rotorcraft airframe crash testbed (TRACT 1) full-scale crash test / / Martin S. Annett [and five others]
| Evaluation of the first transport rotorcraft airframe crash testbed (TRACT 1) full-scale crash test / / Martin S. Annett [and five others] |
| Autore | Annett Martin S. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2014 |
| Descrizione fisica | 1 online resource (61 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Rotary wing aircraft
Crashworthiness Impact loads Energy absorption CH-46 helicopter |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Evaluation of the first transport rotorcraft airframe crash testbed |
| Record Nr. | UNINA-9910703730603321 |
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Annett Martin S.
|
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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