Validation Solution of Incompressible Viscous Flow Over Multi-Element Airfoil
| المصدر: | المجلة الجامعة |
|---|---|
| الناشر: | جامعة الزاوية - مركز البحوث والدراسات العليا |
| المؤلف الرئيسي: | Gabbasa, Asya A. (Author) |
| مؤلفين آخرين: | Assaleh, Tarak (Co-Author) , Dabbashi, Siddig (Co-Author) |
| المجلد/العدد: | مج21, ع3 |
| محكمة: | نعم |
| الدولة: |
ليبيا |
| التاريخ الميلادي: |
2019
|
| الشهر: | مايو |
| الصفحات: | 19 - 30 |
| رقم MD: | 1264368 |
| نوع المحتوى: | بحوث ومقالات |
| اللغة: | الإنجليزية |
| قواعد المعلومات: | EduSearch, EcoLink, IslamicInfo, AraBase, HumanIndex |
| مواضيع: | |
| كلمات المؤلف المفتاحية: |
Fluid Mechanics | Naiver-Stokes Equations | Viscous Fluid Flow
|
| رابط المحتوى: |
الناشر لهذه المادة لم يسمح بإتاحتها. |
| المستخلص: |
Computation fluid dynamics (CFD) simulations are very important tools, which use algorithms and numerical methods for analyzing and solving problems in fluid mechanics. Computer programs are adopted in order to simulate the interaction between gases and liquids with boundary conditions. The programs have the ability to undertake speedy and accurate simulations of complex scenarios, which include turbulent and transonic flows. This paper aims to study an incompressible, viscous, turbulent flow over multi-element airfoils. The governing equations (NS) are solved by using k-epsilon model and SIMPLE algorithm turbulent, steady-state, incompressible flow using the commercial code ANSYS Fluent. Detailed studies are done at different angle of attack flight conditions. By using k-epsilon model and simple algorithm we have obtained the accurate results; that is successful in comparing with wind tunnel results of NACA23012 |
|---|
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