کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
777813 1463819 2010 11 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Fatigue crack growth from flaws in combat aircraft
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی مکانیک
پیش نمایش صفحه اول مقاله
Fatigue crack growth from flaws in combat aircraft
چکیده انگلیسی

The 1969 in-flight failure of an F-111 wing due to the presence of a rogue manufacturing flaw precipitated the adoption of the damage tolerance aircraft design philosophy by the United States Air Force. This article compares this flaw to several flaws or initiating discontinuities that led to unexpected failures in combat-type aircraft operated by the RAAF and found these to be in general an order of magnitude smaller. Failure in the RAAF examples considered here were also dependent upon several other design and production factors in-addition to the initial discontinuity size.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: International Journal of Fatigue - Volume 32, Issue 4, April 2010, Pages 639–649
نویسندگان
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