مشخصات پژوهش

عنوان	Crack Identification in Helicopter Main Blade
نوع پژوهش	مقاله ارائه شده کنفرانسی
کلیدواژه‌ها	Crack identification, Genetic Algorithm, Finite Element Method, Experimental Modal Analysis, Blade
چکیده	In this paper a method for crack detection in blades is presented. In the suggested method, the process of crack identification is consists of four stages. The first stage, three natural frequencies of a blade for different locations and depths of cracks were calculated using Finite Element Method (FEM).
پژوهشگران	مهدی کریمی (نفر اول)، نیما حق شناس (نفر دوم)، فرشید بازمی (نفر سوم)