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.
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