Skip to main content

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)
$257.39 NZD
PDF ( Single user document)
$0.00 NZD
Pages: 12

Related Information

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

Pages: 12