BS EN 2155-13:1993
Current
Date published:
Test methods for transparent materials for aircraft glazing, Determination of temperature at deflection under load
Specifies a procedure for determining the temperature at which an arbitrary deformation occurs when the specimens are subjected to arbitrary bending loads, under conditions of continually rising temperatures.
| Get this standard | Prices exclude GST | |
|---|---|---|
| PDF ( Single user document) |
$239.76 NZD
|
|
| HardCopy |
$239.76 NZD
|
|
Related Information
49.045 Structure and structure elements
Similar Standards
-
BS 185-3:1969
Glossary of aeronautical and astronautical terms, Structures
-
BS 2C 8:1988
Specification for rail and stud configuration for aircraft passenger equipment and cargo restraint
-
BS EN 2155-12:1997
Specification for test methods for transparent materials for aircraft glazing, Determination of linear thermal expansion
-
BS EN 2155-14:1993
Test methods for transparent materials for aircraft glazing, Determination of the 1/10 Vicat softening temperature
BS EN 2155-13:1993
Get this standard
Prices exclude GST
PDF
( Single user document)
$239.76 NZD
HardCopy
$239.76 NZD