A DEVICE FOR IMPLEMENTING THE STRAIN GAGE-HOLE DRILLING METHOD OF RESIDUAL STRESS MEASUREMENT ON AIRCRAFT TRANSPARENCIES

A DEVICE FOR IMPLEMENTING THE STRAIN GAGE-HOLE DRILLING METHOD OF RESIDUAL STRESS MEASUREMENT ON AIRCRAFT TRANSPARENCIES

Crazing of the outer acrylic ply of laminated aircraft transparency systems results in a significant number of canopy or windshield changeouts annually. To understand the mechanisms of craze, and thereby increase transparency durability, current efforts are focusing on relating laboratory craze data...

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Veröffentlicht in:Experimental techniques (Westport, Conn.) Conn.), 1993-07, Vol.17 (4), p.25-30
Hauptverfasser: Whitney, T.J., Stenger, G.J.
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container_title Experimental techniques (Westport, Conn.)
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creator Whitney, T.J.
Stenger, G.J.
description Crazing of the outer acrylic ply of laminated aircraft transparency systems results in a significant number of canopy or windshield changeouts annually. To understand the mechanisms of craze, and thereby increase transparency durability, current efforts are focusing on relating laboratory craze data to field data from removed canopies. A number of factors are seen to contribute to craze, including exposure to chemicals, temperature, and stress in the material.
doi_str_mv 10.1111/j.1747-1567.1993.tb00759.x
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title A DEVICE FOR IMPLEMENTING THE STRAIN GAGE-HOLE DRILLING METHOD OF RESIDUAL STRESS MEASUREMENT ON AIRCRAFT TRANSPARENCIES
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