Evaluating Impact Damage of Flat Composite Plate for Surrogate Bird-Strike Testing of Aeroengine Fan Blade
نویسندگان
چکیده
Bird-strike failure of fan blades is one the basic challenges for safety aircraft engines. Simplified flat blade-like plates are always used damage mechanism study composite laminates. One undesirable issue at root clamped under high-velocity impact. For this purpose, two different strategies were exploited to obtain desirable impact distributions, namely location and boundary condition. Numerical models simplified plate bird projectile constructed by using finite element method (FEM) smoothed particle hydrodynamics (SPH) approaches. The distributions comparatively investigated in detail. numerical results show that changing condition most effective way preferable damages further analysis real blades. Present will be useful future surrogate experimental design bird-strike testing.
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چکیده هدف اصلی از طراحی لرزه ای تامین ایمنی جانی در هنگام وقوع زلزله و تعمیر پذیر بودن سازه خسارت دیده، پس از وقوع زلزله است. تجربه زلزله های اخیر نشان داده است که ساختمان های طراحی شده با آیین نامه های مبتنی بر نیرو از نظر محدود نمودن خسارت وارده بر سازه دقت لازم را ندارند. این امر سبب پیدایش نسل جدید آیین نامه های مبتنی بر عملکرد شده است. در این آیین نامه ها بر اساس تغییرشکل های غیرارتجاعی ...
15 صفحه اولInternational Bird Strike Committee
Aircraft repeatedly prove that birds and aircraft cannot occupy the same airspace at the same time. In an average year about 3000 birdstrikes cause 50-80 million US dollars in damage to USAF aircraft. To the worldwide aviation fleet this problem is estimated to cost more than three billion US dollars per year. Factors for consideration in establishing birdstrike resistance requirements, and in ...
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ژورنال
عنوان ژورنال: Journal of composites science
سال: 2021
ISSN: ['2504-477X']
DOI: https://doi.org/10.3390/jcs5070171