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Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure / / C.E. Harris [and three others]
| Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure / / C.E. Harris [and three others] |
| Autore | Harris Charles E. <1950-> |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1996 |
| Descrizione fisica | 1 online resource (25 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Fuselages
Residual strength Crack initiation Crack propagation Fatigue (materials) Computer programs |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707911903321 |
Harris Charles E. <1950->
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications [[electronic resource] /] / A.T. Nettles
| A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications [[electronic resource] /] / A.T. Nettles |
| Autore | Nettles A. T (Alan T.) |
| Pubbl/distr/stampa | Huntsville, Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011] |
| Descrizione fisica | 1 online resource (vii, 39 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Compressive strength
Impact strength Honeycomb structures Launch vehicles Damage Tolerances (mechanics) Residual strength |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701853303321 |
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Nettles A. T (Alan T.)
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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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The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles [[electronic resource] /] / A.T. Nettles, A.J. Hodge, and J.R. Jackson
| The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles [[electronic resource] /] / A.T. Nettles, A.J. Hodge, and J.R. Jackson |
| Autore | Nettles A. T (Alan T.) |
| Pubbl/distr/stampa | [Huntsville], Ala. : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , [2011] |
| Descrizione fisica | 1 online resource (vii, 23 pages) : illustrations |
| Altri autori (Persone) |
HodgeA. J
JacksonJ. R |
| Collana | NASA/TP |
| Soggetto topico |
Damage assessment
Launch vehicles Thermal protection Sandwich structures Residual strength Ares 1 launch vehicle Composite structures Composite materials Impact damage |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910700761103321 |
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Nettles A. T (Alan T.)
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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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Progressive Damage Analysis of Laminated Composite (PDALC) : a computational model implemented in the NASA COMET finite element code / / David C. Lo [and three others]
| Progressive Damage Analysis of Laminated Composite (PDALC) : a computational model implemented in the NASA COMET finite element code / / David C. Lo [and three others] |
| Autore | Lo David C. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1996 |
| Descrizione fisica | 1 online resource (41 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Laminated materials - Cracking - Mathematical models
Composite materials - Cracking - Mathematical models Finite element method - Data processing Residual strength Structural analysis Matrix materials Cracking (fracturing) Damage assessment |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Progressive Damage Analysis of Laminated Composite |
| Record Nr. | UNINA-9910704399103321 |
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Lo David C.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A progressive damage methodology for residual strength predictions of notched composite panels / / Timothy W. Coats and Charles E. Harris
| A progressive damage methodology for residual strength predictions of notched composite panels / / Timothy W. Coats and Charles E. Harris |
| Autore | Coats Timothy W. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , June 1998 |
| Descrizione fisica | 1 online resource (43 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Composite structures
Crack propagation Epoxy matrix composites Fractography Fracture mechanics Fracture strength Laminates Loads (forces) Residual strength |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705871503321 |
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Coats Timothy W.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , June 1998 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Residual strength analyses of riveted lap-splice joints / / B.R. Seshadri and J.C Newman, Jr
| Residual strength analyses of riveted lap-splice joints / / B.R. Seshadri and J.C Newman, Jr |
| Autore | Seshadri B. R. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2000 |
| Descrizione fisica | 1 online resource (24 pages) : illustrations, some color |
| Collana | NASA/TM |
| Soggetto topico |
Lap joints
Riveted joints Structural analysis Rivets Cracks Crack propagation Fracturing Holes (mechanics) Residual strength Computer programs |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706222003321 |
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Seshadri B. R.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2000 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Simulation studies for surfaces and materials strength [[electronic resource] ] : semiannual progress report for cooperative agreement NCC2-297 for the period November 1, 1986 - April 30, 1987 / / prepared by Eloret Institute ; Timur Halicioglu ; principal investigator
| Simulation studies for surfaces and materials strength [[electronic resource] ] : semiannual progress report for cooperative agreement NCC2-297 for the period November 1, 1986 - April 30, 1987 / / prepared by Eloret Institute ; Timur Halicioglu ; principal investigator |
| Autore | Halicioglu Timur <1935-> |
| Pubbl/distr/stampa | Palo Alto, CA : , : Eloret Instititute |
| Descrizione fisica | 7 pages, 5 unnumbered pages ; ; 28 cm |
| Collana | NASA-CR |
| Soggetto topico |
Molecular dynamics
Computerized simulation Materials handling Residual strength Surface properties |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Simulation studies for surfaces and materials strength |
| Record Nr. | UNINA-9910698969503321 |
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Halicioglu Timur <1935->
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| Palo Alto, CA : , : Eloret Instititute | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Stressed oxidation of C/SiC composites / / Michael C. Halbig [and three others]
| Stressed oxidation of C/SiC composites / / Michael C. Halbig [and three others] |
| Autore | Halbig Michael C. <1969-> |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center : , : U.S. Army Research Laboratory, , April 1997 |
| Descrizione fisica | 1 online resource (8 pages) : illustrations |
| Collana |
NASA technical memorandum
Army research laboratory technical report |
| Soggetto topico |
Oxidation
Ceramics High temperature tests Microstructure Fiber-matrix interfaces Debonding (materials) Ceramic matrix composites Residual strength Microcracks |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Stressed oxidation of carbon fiber-reinforced silicon carbide composites |
| Record Nr. | UNINA-9910707607503321 |
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Halbig Michael C. <1969->
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center : , : U.S. Army Research Laboratory, , April 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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