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A comparison of tension and compression creep in a polymeric composite and the effects of physical aging on creep / / Thomas S. Gates, David R. Veazie, L. Catherine Brinson
| A comparison of tension and compression creep in a polymeric composite and the effects of physical aging on creep / / Thomas S. Gates, David R. Veazie, L. Catherine Brinson |
| Autore | Gates Thomas S. <1959-> |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1996 |
| Descrizione fisica | 1 online resource (33 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Aging (materials)
Compression loads Creep tests Shear creep Tensile tests Compression tests Polymer matrix composites Fiber composites Tension |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910690471903321 |
Gates Thomas S. <1959->
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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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Rate dependent stress-strain behavior of advanced polymer matrix composites / / Thomas S. Gates
| Rate dependent stress-strain behavior of advanced polymer matrix composites / / Thomas S. Gates |
| Autore | Gates Thomas S. <1959-> |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 1991 |
| Descrizione fisica | 1 online resource (approximately 28 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Composite materials
Creep properties Viscoplasticity |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717006503321 |
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Gates Thomas S. <1959->
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 1991 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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