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Acoustically tailored composite rotorcraft fuselage panels / / Stephen Hambric [and eight others]
| Acoustically tailored composite rotorcraft fuselage panels / / Stephen Hambric [and eight others] |
| Autore | Hambric Stephen A. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2015 |
| Descrizione fisica | 1 online resource (iii, 153 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Acoustic propagation
Rotary wing aircraft Sandwich structures Sound transmission Noise reduction |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703966003321 |
Hambric Stephen A.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP) [[electronic resource] /] / Joanne L. Walsh ... [and others]
| Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP) [[electronic resource] /] / Joanne L. Walsh ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2005] |
| Descrizione fisica | 1 online resource (113 pages) : color illustrations |
| Altri autori (Persone) | WalshJoanne L |
| Collana | NASA TP- |
| Soggetto topico |
Body-wing configurations
Canard configurations Aeroelasticity Sandwich structures Longitudinal control Design analysis Composite materials |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aeroelastic sizing for high-speed research |
| Record Nr. | UNINA-9910701389603321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2005] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates [[electronic resource] /] / Alexander Tessler ... [and others]
| Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates [[electronic resource] /] / Alexander Tessler ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] |
| Descrizione fisica | 1 online resource (19 pages) : illustrations |
| Altri autori (Persone) | TesslerAlexander |
| Collana | NASA/TP |
| Soggetto topico |
Composite structures
Laminates Sandwich structures Shear stress Computational mechanics Finite element method |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702003703321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders / / Michael P. Nemeth
| An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders / / Michael P. Nemeth |
| Autore | Nemeth Michael P. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013 |
| Descrizione fisica | 1 online resource (60 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Anisotropy
Axial compression loads Cylindrical shells Inhomogeneity Laminates Sandwich structures |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704816303321 |
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Nemeth Michael P.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel / / David E. Myers, Evan J. Pineda [and four others]
| Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel / / David E. Myers, Evan J. Pineda [and four others] |
| Autore | Myers David E (Engineer) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013-2014 |
| Descrizione fisica | 1 online resource (3 volumes) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Fibrous composites
Finite element method Honeycomb structures Ares 5 cargo launch vehicle Epoxy matrix composites Fiber composites Robustness (mathematics) Sandwich structures |
| Soggetto genere / forma |
Technical reports.
Ebook |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 1. 8-ply in-autoclave facesheets -- pt. 2. 6-ply in-autoclave facesheets -- pt. 3. 8-ply out-of-autoclave facesheets. |
| Record Nr. | UNINA-9910705251203321 |
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Myers David E (Engineer)
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013-2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 |
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Hodge A. J
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| [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Composite Crew Module (CCM) permeability characterization / / Michael T. Kirsch
| Composite Crew Module (CCM) permeability characterization / / Michael T. Kirsch |
| Autore | Kirsch Michael T. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , [2013] |
| Descrizione fisica | 1 online resource (39 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Leading edges
Spacecraft modules Honeycomb structures Composite structures Sandwich structures Shells (structural forms) Linings Permeability Leakage Carbon fiber reinforced plastics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Composite Crew Module |
| Record Nr. | UNINA-9910704815803321 |
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Kirsch Michael T.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , [2013] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Composite sandwich structure and method for making same [[electronic resource] /] / inventor, Charles J. Magurany
| Composite sandwich structure and method for making same [[electronic resource] /] / inventor, Charles J. Magurany |
| Edizione | [[Redacted ed.]] |
| Pubbl/distr/stampa | [Washington, DC] : , : [National Aeronautics and Space Administration], , [1995] |
| Descrizione fisica | 1 online resource : illustrations |
| Altri autori (Persone) | MaguranyCharles J |
| Collana | NASA case |
| Soggetto topico |
Composite structures
Fabrication Laminates Ribs (supports) Sandwich structures Composite construction |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697270703321 |
| [Washington, DC] : , : [National Aeronautics and Space Administration], , [1995] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Compression after impact experiments and analysis on honeycomb core sandwich panels with thin facesheets [[electronic resource] /] / Thomas D. McQuigg
| Compression after impact experiments and analysis on honeycomb core sandwich panels with thin facesheets [[electronic resource] /] / Thomas D. McQuigg |
| Autore | McQuigg Thomas D |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] |
| Descrizione fisica | 1 online resource (xxvii, 258 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Composite structures
Impact damage Honeycomb cores Sandwich structures Damage Compression loads |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701159403321 |
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McQuigg Thomas D
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Compression response of a sandwich fuselage keel panel with and without damage / / David M. McGowan and Damodar R. Ambur
| Compression response of a sandwich fuselage keel panel with and without damage / / David M. McGowan and Damodar R. Ambur |
| Autore | McGowan David M. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 1997 |
| Descrizione fisica | 1 online resource (33 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Composite structures
Finite element method Fuselages Graphite-epoxy composites Honeycomb cores Impact damage Sandwich structures |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707910803321 |
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McGowan David M.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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