EN 6031:2015
Current
The latest, up-to-date edition.
Aerospace series - Fibre reinforced plastics - Test method - Determination of in-plane shear properties (± 45° tensile test)
25-11-2015
European foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Principle of the method
5 Designation of the method
6 Apparatus
7 Test specimen
8 Procedure
9 Presentation of the results
10 Test report
This European Standard specifies the procedure for the determination of the in-plane shear strength and modulus of fibre composites. The procedure is based on the uni-axial tensile stress-strain response of a 45° laminate which is symmetrically laminated about the mid-plane.This standard is applicable to composite laminates manufactured from unidirectional tape or woven fabric reinforcement.This standard does not give any directions necessary to meet the health and safety requirements. It is the responsibility of the user of this standard to consult and establish appropriate health and safety precautions.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 6031. (12/2015)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| NF EN 6031 : 2017 | Identical |
| NBN EN 6031 : 2015 | Identical |
| NEN EN 6031 : 2015 | Identical |
| NS EN 6031 : 2015 | Identical |
| I.S. EN 6031:2015 | Identical |
| PN EN 6031 : 2016 | Identical |
| UNI EN 6031 : 2016 | Identical |
| UNE-EN 6031:2015 | Identical |
| BS EN 6031:2015 | Identical |
| DIN EN 6031:2016-02 | Identical |
| 93/706616 DC : 0 | PREN 2833-1 - AEROSPACE SERIES - TECHNICAL SPECIFICATION - GLASS FIBER THERMOSETTING PREIMPREGNATES - PART 1: GENERAL |
| SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| SAE AMS 2980/1 : 2014 | CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL - PART 1 - GENERAL REQUIREMENTS |
| 95/714421 DC : 0 | PREN 2833-3 - AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 3: GLASS FABRIC/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 180 DEGREE C FOR CONTINUOUS USE UP TO 120 DEGREE C |
| SAE AMS 3970/6 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 6 - MATERIAL SPECIFICATION: CARBON FIBER FABRIC REINFORCED EPOXY PREPREG FOR REPAIR, PLAIN WEAVE FABRIC, 193 G/M[2], ADHESIVE FILM FOR REPAIR AND NON-STRUCTURAL GLASS FIBER FABRIC REINFORCED EPOXY PREPREG, 105 G/M[2] |
| 95/714422 DC : 0 | PREN 2833-4 - AEROSPACE SERIES - GLASS FIBER THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREE C FOR CONTINUOUS USE UP TO 80 DEGREE C |
| PREN 2833-4 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
| EN 2565:2013 | Aerospace series - Preparation of carbon fibre reinforced resin panels for test purposes |
| EN 2489:1995 | Aerospace series - Fibre reinforced plastics - Determination of the action of test fluids |
| PREN 2823 : 200P2 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - DETERMINATION OF THE EFFECT OF EXPOSURE TO HUMID ATMOSPHERE ON PHYSICAL AND MECHANICAL CHARACTERISTICS |
| EN 2743:2001 | Aerospace series - Fibre reinforced plastics - Standard procedures for conditioning prior to testing unaged materials |
| EN 2374:1991 | Aerospace series - Glass fibre reinforced mouldings and sandwich composites - Production of test panels |
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