کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
291719 509776 2008 21 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Assessment of uncertainty in response estimation for turbine engine bladed disks
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی عمران و سازه
پیش نمایش صفحه اول مقاله
Assessment of uncertainty in response estimation for turbine engine bladed disks
چکیده انگلیسی

Stress prediction in turbine blades is affected by limitations in the measurement setup as well as by various sources of uncertainty in the model-based inference techniques. The presence of uncertainty diminishes the confidence in the estimated response, whose fidelity lowers further when results are extrapolated to operating conditions or systems other than the tested ones. A procedure is being developed with a twofold objective: maximization, under given computational constraints, of a system's model accuracy and quantification of any remaining uncertainty associated with the estimation technique. A probabilistic analysis, in which uncertainties are explicitly modeled has been carried out to investigate the effects of modeling and input parameter uncertainties, and to evaluate their contribution to a system's vibratory response prediction. Results and considerations are herein described and discussed.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Journal of Sound and Vibration - Volume 317, Issues 3–5, 11 November 2008, Pages 625–645
نویسندگان
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