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Design, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners [[electronic resource] /] / Wesley C.H. Slemp ... [and others]
| Design, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners [[electronic resource] /] / Wesley C.H. Slemp ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] |
| Descrizione fisica | 1 online resource (39 pages) : illustrations (some color) |
| Altri autori (Persone) | SlempWesley C. H |
| Collana | NASA/TP |
| Soggetto topico |
Buckling
Finite element method Design optimization Load tests Elastic buckling Wing panels Fixtures Deflection Loads (forces) |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701449703321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Fracture mechanics analyses of the slip-side joggle regions of wing-leading-edge panels [[electronic resource] /] / Ivatury S. Raju ... [and others]
| Fracture mechanics analyses of the slip-side joggle regions of wing-leading-edge panels [[electronic resource] /] / Ivatury S. Raju ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] |
| Descrizione fisica | 1 online resource (iv, 20 pages) : color illustrations |
| Altri autori (Persone) | RajuI. S |
| Collana | NASA/TM |
| Soggetto topico |
Carbon-carbon composites
Fracture mechanics Space shuttles Wing panels Leading edges; wings |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910700303603321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Fuel containment, lightning protection, and damage tolerance in large composite primary aircraft structures / / Charles F. Griffin and Arthur M. James
| Fuel containment, lightning protection, and damage tolerance in large composite primary aircraft structures / / Charles F. Griffin and Arthur M. James |
| Autore | Griffin C. F (Charles Francis), <1944-> |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , May 1985 |
| Descrizione fisica | 1 online resource (ix, 31 pages) : illustrations |
| Collana | NASA contractor report |
| Soggetto topico |
Aircraft structures
Fuel tanks Graphite-epoxy composites Impact tolerances Lightning suppression Wing panels |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706296303321 |
Griffin C. F (Charles Francis), <1944->
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , May 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Thermostructural evaluation of joggle region on the shuttle orbiter's wing leading edge [[electronic resource] /] / Sandra P. Walker and Jerry E. Warren
| Thermostructural evaluation of joggle region on the shuttle orbiter's wing leading edge [[electronic resource] /] / Sandra P. Walker and Jerry E. Warren |
| Autore | Walker Sandra P |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] |
| Descrizione fisica | 1 online resource (28 pages) : illustrations (some color) |
| Altri autori (Persone) | WarrenJerry E |
| Collana | NASA/TM |
| Soggetto topico |
Leading edges
Mathematical models Space Shuttle orbiters Wing panels Spallation Coatings Carbon-carbon composites Thermodynamic properties |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702004103321 |
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Walker Sandra P
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Titanium honeycomb panel testing / / W. Lance Richards, Randolph C. Thompson
| Titanium honeycomb panel testing / / W. Lance Richards, Randolph C. Thompson |
| Autore | Richards W. Lance |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , October 1996 |
| Descrizione fisica | 1 online resource (17 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Honeycomb structures
Wing panels Hypersonic vehicles Structural analysis Nondestructive tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704381203321 |
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Richards W. Lance
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , October 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
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Wing panels
(5)
- Carbon-carbon composites (2)
- Aircraft structures (1)
- Buckling (1)
- Coatings (1)