NFL 17 19956 : 1995
Current
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The latest, up-to-date edition.
AIRCRAFT INDUSTRY - SYNTHETIC CLOTHS FOR THE FABRIC OF AIRPLANE STRUCTURES - DETERMINATION OF THE LOAD AND ELONGATION AT RUPTURE BY TENSILE TESTING OF CLOTHS IN DELIVERY CONDITION AND OF FREE COATED CLOTHS
Published date
12-01-2013
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| DevelopmentNote |
Indice de classement: L17-956. (12/2007)
|
| DocumentType |
Standard
|
| PublisherName |
Association Francaise de Normalisation
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| Status |
Current
|
| NFL 17 19951 : 1995 | AIRCRAFT INDUSTRY - SYNTHETIC CLOTHS FOR THE FABRIC OF AIRPLANE STRUCTURES - DETERMINATION OF THE MECHANICAL CHARACTERISTICS AFTER WEATHERING |
| NFL 17 19953 : 1995 | AIRCRAFT INDUSTRY - SYNTHETIC CLOTHS FOR THE FABRIC OF AIRPLANE STRUCTURES - DETERMINATION OF SHEAR STRENGTH BY STRETCHING CLOTHS, IN THE DELIVERY CONDITION, STUCK THEN PROTECTED BEFORE AND AFTER AGING |
| NFL 17 19950 : 1995 | AIRCRAFT INDUSTRY - SYNTHETIC CLOTHS FOR THE FABRIC OF AIRPLANE STRUCTURES - REALIZATION OF TEST PANELS |
| ISO 5081:1977 | Textiles Woven fabrics Determination of breaking strength and elongation (Strip method) |
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