|
[Sponsors] |
![]() |
![]() |
#1 |
Member
Join Date: Apr 2016
Posts: 53
Rep Power: 9 ![]() |
Hi all,
I hope you all are doing well. I am working on the simulation of airfoils with boundary layer suction. I found a reference to validate my CFD results, as shown below. "Stanewsky E, Délery J, Fulker J, de Matteis P, editors. Drag Reduction by Shock and Boundary Layer Control: Results of the Project EUROSHOCK II. Supported by the European Union 1996-1999. Springer Science & Business Media; 2002 Apr 24." They used RAE 5225 airfoil, but its coordinates were not given explicitly. Kindly share it with me if anybody has the coordinates. Also, please feel free to suggest any other references which contain detailed experimental data of boundary layer suction on airfoil shapes. Thanks in advance. |
|
![]() |
![]() |
![]() |
Tags |
airfoil 2d, boundary layer control, cfd analysis, coordinate files, suction |
Thread Tools | Search this Thread |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
SU2 AOA optimization | 454514566@qq.com | SU2 | 9 | March 7, 2022 16:17 |
Ffd_control_point_2d | feiyi | SU2 | 4 | September 30, 2019 12:42 |
High drag for airfoil compared to XFOIL and wind tunnel data | Ry10 | SU2 | 15 | October 30, 2016 17:27 |
2D FFD Optimization | RLangtry | SU2 | 2 | August 5, 2014 09:48 |
Problem with restart solution in shape_optimization.py | robyTKD | SU2 Shape Design | 21 | May 29, 2013 09:26 |