کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
4993317 1457618 2016 9 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Empirical modelling of noise from high aspect ratio rectangular jets
ترجمه فارسی عنوان
مدلسازی تجربی از نویز از جت های مستطیلی نسبتا بزرگ
کلمات کلیدی
سر و صدای جت، قوانین مقیاس جرثقیل سر و صدا، جت بزرگ نسبت ابعاد، جت مستطیلی،
موضوعات مرتبط
مهندسی و علوم پایه مهندسی شیمی جریان سیال و فرایندهای انتقال
چکیده انگلیسی
Noise measurements have been performed on rectangular jets of aspect ratios ranging from 49 to 987 with the aim of determining the appropriate velocity and length scaling to be used in an empirical noise prediction model. The results have shown that the velocity exponent is a function of the nozzle aspect ratio, decreasing with increasing nozzle aspect ratio. In an effort to establish a general prediction model, the velocity exponent of 7 was chosen as the best compromise to represent all the measured data. The analysis of the noise measurements from high aspect ratio nozzles of varying jet height and width has shown that, for the range of aspect ratios considered, the jet sound power level scales with the nozzle height to the power of 3 and the nozzle width to the power of 1. The derived jet noise scaling has been validated with independent experimental data and shows good agreement.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: International Journal of Heat and Fluid Flow - Volume 62, Part A, December 2016, Pages 1-9
نویسندگان
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