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Annealing effects on creep and rupture of polycrystalline alumina-based fibers / / J.C. Goldsby [and three others]
| Annealing effects on creep and rupture of polycrystalline alumina-based fibers / / J.C. Goldsby [and three others] |
| Autore | Goldsby Jon C. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1998 |
| Descrizione fisica | 1 online resource (11 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Annealing
Rupturing Creep strength Fiber composites Ceramic fibers Tensile creep Aluminum oxides Reinforcing fibers |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706194803321 |
Goldsby Jon C.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1998 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Creep and rupture strength of an advanced CVD SiC fiber / / J.C. Goldsby, H.M. Yun, James A. DiCarlo
| Creep and rupture strength of an advanced CVD SiC fiber / / J.C. Goldsby, H.M. Yun, James A. DiCarlo |
| Autore | Goldsby Jon C. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , April 1997 |
| Descrizione fisica | 1 online resource (6 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Creep rupture strength
Creep properties Creep strength Tensile creep Polycrystals Morphology Fiber strength Annealing Fracture strength |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Creep and rupture strength of an advanced chemically vapor deposited silicon carbide fiber |
| Record Nr. | UNINA-9910707309703321 |
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Goldsby Jon C.
|
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , April 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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