AECMA PREN 2155-12-1981 Test Methods for Transparent Materials for Aircraft Glazing - Part 12 - Determination of Linear Thermal Expansion Aerospace Series Edition 1
This standard specifies the requirements relating to clad sheet and strip, in aluminium alloy AL-P2024-,
for use in the T351 condition, 0,8 mm I a 2 6 mm, for aerospace applications.
The material is manufactured to a minimum residual stress requirement, for chemical milling applications.
AECMA PREN 2155-12-1981 history
1981AECMA PREN 2155-12-1981 Test Methods for Transparent Materials for Aircraft Glazing - Part 12 - Determination of Linear Thermal Expansion Aerospace Series Edition 1