کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1718163 1520101 2013 6 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Study on shock wave-vortex ring interaction by the micro vortex generator controlled ramp flow with turbulent inflow
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Study on shock wave-vortex ring interaction by the micro vortex generator controlled ramp flow with turbulent inflow
چکیده انگلیسی

In this study, we will investigate the interaction between the vortex rings and oblique shocks generated by the micro vortex generatorʼs (MVG) controlled ramp flow at M=2.5M=2.5 and Reθ=5760Reθ=5760. An implicit large eddy simulation method is used by solving the unfiltered form of the Navier–Stokes equations with the 5th order bandwidth-optimized WENO scheme. It shows that the vortex ring structure generated by MVG is very stable, it does not break down and it keeps its original topology after penetrating the strong shock wave. However, the oblique shocks are broken when they interact with vortex rings. The bump on the 3D shock wave surface is observed and its mechanism is explained. The separation zone, which is originally generated by the shock–boundary layer interaction, is significantly reduced due to the vortex ring–shock interaction.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 30, Issue 1, October 2013, Pages 226–231
نویسندگان
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