Abstract:Owing to the inadequacy of conventional laboratory windshield qualification testing methods, it is not unusual for unforeseen problems to develop in the real world of flight service. Aircraft windshields are normally subjected to static, material, environmental, and, in some instances, to limited service condition testing before being incorporated into prototype hardware. In‐service monitoring is used to compare the prototype to previous designs. Determining the relative effectiveness of corrective “fixes” or … Show more
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