کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
9690578 1457333 2005 21 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Experimental investigation of 3D acoustic receptivity of an airfoil boundary layer due to surface vibrations
موضوعات مرتبط
مهندسی و علوم پایه مهندسی شیمی جریان سیال و فرایندهای انتقال
پیش نمایش صفحه اول مقاله
Experimental investigation of 3D acoustic receptivity of an airfoil boundary layer due to surface vibrations
چکیده انگلیسی
The receptivity was investigated in two general cases: in 'plus-regimes' when the TS-waves were excited at combination frequencies fTS+=fac+fv and in 'minus-regimes' when the excitation occurred at frequencies fTS−=fac−fv. The complex (amplitude and phase) receptivity coefficients are obtained experimentally as functions of the spanwise wavenumber (and the wave propagation angle) for three different frequency ratios K and also for several TS-wave frequencies at fixed values of K. The obtained vibro-acoustic receptivity coefficients are compared with the acoustic-roughness receptivity coefficients (i.e. for K=0) found in previous experiments and DNS.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: European Journal of Mechanics - B/Fluids - Volume 24, Issue 5, September–October 2005, Pages 621-641
نویسندگان
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