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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 |
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 test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02: test dates: 3-6 February 2009 / / Mark W. Hilburger [and three others]
| Buckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02: test dates: 3-6 February 2009 / / Mark W. Hilburger [and three others] |
| Autore | Hilburger Mark W (Mark William) |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2017 |
| Descrizione fisica | 1 online resource (x, 91 pages) : color illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Buckling
Compression loads Cylindrical shells Launch vehicles Aluminum alloys |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Buckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02 |
| Record Nr. | UNINA-9910705705003321 |
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Hilburger Mark W (Mark William)
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The exact solution for linear thermoelastic axisymmetric deformations of generally laminated circular cylindrical shells / / Michael P. Nemeth and Marc R. Schultz
| The exact solution for linear thermoelastic axisymmetric deformations of generally laminated circular cylindrical shells / / Michael P. Nemeth and Marc R. Schultz |
| Autore | Nemeth Michael P. |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] |
| Descrizione fisica | 1 online resource (99 pages) : color illustrations |
| Collana | [NASA technical paper] |
| Soggetto topico |
Anisotropy
Cylindrical shells Boundary conditions Composite structures Surface temperature Temperature distribution Thermoelasticity Laminates Axial strain |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702094303321 |
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Nemeth Michael 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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The influence of lamination angles on the interior noise levels of an aircraft / / Christian M. Fernholz, Jay H. Robinson
| The influence of lamination angles on the interior noise levels of an aircraft / / Christian M. Fernholz, Jay H. Robinson |
| Autore | Fernholz Christian M (Christian Michael) |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1996 |
| Descrizione fisica | 1 online resource (vi, 83 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Aircraft production
Cylindrical shells Equations of motion Finite element method Frequency ranges Thin walled shells Structural design criteria Noise reduction Noise intensity Laminates |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707240203321 |
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Fernholz Christian M (Christian Michael)
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Pre-test analysis predictions for the shell buckling knockdown factor checkout tests, TA01 and TA02 [[electronic resource] /] / Robert P. Thornburgh, Mark W. Hilburger
| Pre-test analysis predictions for the shell buckling knockdown factor checkout tests, TA01 and TA02 [[electronic resource] /] / Robert P. Thornburgh, Mark W. Hilburger |
| Autore | Thornburgh Robert P |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] |
| Descrizione fisica | 1 online resource (vii, 37 pages) : color illustrations |
| Altri autori (Persone) | HilburgerMark W (Mark William) |
| Collana | NASA/TM |
| Soggetto topico |
Structural analysis
Lithium alloys Shell stability Cylindrical shells Aluminum alloys Loads (forces) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910700303703321 |
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Thornburgh Robert P
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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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Soggetto topico
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Cylindrical shells
(5)
- Laminates (3)
- Aluminum alloys (2)
- Anisotropy (2)
- Aircraft production (1)