کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1719444 1520189 2010 13 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Algebraic turbulent energy flux models for hypersonic shear flows
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Algebraic turbulent energy flux models for hypersonic shear flows
چکیده انگلیسی

Algebraic truncation models were derived for the turbulent energy flux for high-speed shear flows with and without thermal and mechanical non-equilibrium effects. To facilitate closure, fluctuating dilatation moments were modeled via conservation of mass truncations and the inhomogeneous terms were neglected. The resulting energy flux model provided significant improvements, up to 20%, in the temperature predictions over the gradient diffusion model for equilibrium flows over a Mach number range of 0.02–11.8. Our experiments showed that vibrational relaxation significantly altered the basic decay rate of grid turbulence. Also, our models indicated that compressibility introduces an explicit pressure gradient dependency. Analyses of a governing parameter indicated that these terms are negligibly small for low speeds, but may be important, or even dominant, for high-speed flows.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Progress in Aerospace Sciences - Volume 46, Issues 2–3, February–April 2010, Pages 49–61
نویسندگان
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