کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
5473014 1520070 2017 10 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
An adaptive fully-Lagrangian meshless method for incompressible laminar flow airfoil studies
ترجمه فارسی عنوان
یک روش سازگار به طور کامل لاگرانژ بدون حساسیت برای مطالعات هواپیما جریان هوا غیر متراکم
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
چکیده انگلیسی
Laminar incompressible flow around a NACA0012 airfoil placed in a free-stream at various incidences has been revisited with the use of a fully-Lagrangian meshless method based on a Smoothed Particle Hydrodynamics (SPH) formulation. Spatial adaptivity has been incorporated in the scheme via splitting and merging of SPH particles employing zonal criteria. In addition, a novel algorithm has been proposed here so that particle merging may be achieved, ensuring the robustness, accuracy and efficiency of the computational simulations. The results obtained have been benchmarked against available data from mesh-based methods. Good agreement has been found both in steady and unsteady flow regimes. Overall, the present work demonstrated the effectiveness and competitiveness of this meshfree approach for detailed studies in aerodynamics.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 64, May 2017, Pages 161-170
نویسندگان
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