کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
10681401 | 1013897 | 2005 | 9 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Opportunities for the integrated use of measurements and computations for the understanding of delta wing aerodynamics
دانلود مقاله + سفارش ترجمه
دانلود مقاله ISI انگلیسی
رایگان برای ایرانیان
موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی هوافضا
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: Opportunities for the integrated use of measurements and computations for the understanding of delta wing aerodynamics Opportunities for the integrated use of measurements and computations for the understanding of delta wing aerodynamics](/preview/png/10681401.png)
چکیده انگلیسی
This paper considers the current status of delta wing research from the point of view of the potential for using joint experimental and computational studies to advance the subject. After a brief review of the available measurement and numerical methods, delta wing phenomena are considered in the following categories: shear layer instabilities, vortex breakdown, vortex interactions, non-slender vortices, multiple vortices, manoeuvring wing vortices and vortex/flexible wing interaction. It is concluded that CFD can be very valuable to guide the type and location of experimental data collected and to enhance the understanding of the data. Currently CFD requires more extensive datasets which include boundary layer and flowfield information, and which ideally combine different types of data.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 9, Issue 3, April 2005, Pages 181-189
Journal: Aerospace Science and Technology - Volume 9, Issue 3, April 2005, Pages 181-189
نویسندگان
I. Gursul, M.R. Allan, K.J. Badcock,