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Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.045 Structure and structure elements>BS EN 2155-13:1993 Test methods for transparent materials for aircraft glazing Determination of temperature at deflection under load
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immediate downloadReleased: 1993-04-15
BS EN 2155-13:1993 Test methods for transparent materials for aircraft glazing Determination of temperature at deflection under load

BS EN 2155-13:1993

Test methods for transparent materials for aircraft glazing Determination of temperature at deflection under load

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Standard number:BS EN 2155-13:1993
Pages:12
Released:1993-04-15
ISBN:0 580 22066 4
Status:Standard
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BS EN 2155-13:1993


This standard BS EN 2155-13:1993 Test methods for transparent materials for aircraft glazing is classified in these ICS categories:
  • 49.045 Structure and structure elements

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.