کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1719447 1520189 2010 17 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Viscosity effects on weak irregular reflection of shock waves in steady flow
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Viscosity effects on weak irregular reflection of shock waves in steady flow
چکیده انگلیسی
The viscosity effects on weak shock wave reflection are investigated with the Navier-Stokes and DSMC flow solvers. It is shown that the viscosity plays a crucial role in the vicinity of three-shock intersection. Instead of a singular triple point, in viscous flow there is a smooth three shock transition zone, where one-dimensional shock jump relations cannot be applied. At the flow parameters corresponding to the von Neumann reflection, when no inviscid three-shock solution exists, the computations predict an irregular shock-wave configuration similar to that observed previously in experiments. The existence of a viscous zone in the region of shock-wave interaction allows a continuous transition from the parameters behind the Mach stem to the parameters behind the reflected shock, which is impossible in the inviscid three-shock theory. Results of numerical simulations agree qualitatively with the conclusions of the approximate viscous theory, which describes the flow in the vicinity of the three-shock intersection.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Progress in Aerospace Sciences - Volume 46, Issues 2–3, February–April 2010, Pages 89-105
نویسندگان
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