کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1719563 1520196 2007 22 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Triple-deck theory of supersonic laminar viscous–inviscid interaction due to wall temperature jumps
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Triple-deck theory of supersonic laminar viscous–inviscid interaction due to wall temperature jumps
چکیده انگلیسی

The short-ranged local viscous–inviscid interaction field generated by a wall temperature jump on a flat plate in supersonic flow is studied in detail with an analytical triple-deck model. Treatment of the rapid heat transfer changes both upstream and downstream of the jump is included. Closed-form relationships for the pressure and heating variations, including upstream influence, are derived from triple-deck theory and are found to be in good agreement with numerical solutions of the compressible Navier–Stokes equations. Such relationships not only clarify the interactive physics involved, but also are useful in preliminary design of thermal protection systems and as an insertable module to improve computational fluid dynamics code efficiency when applied to such small-scale interaction problems.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Progress in Aerospace Sciences - Volume 43, Issues 1–3, January–April 2007, Pages 42–63
نویسندگان
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