CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > General Forums > Main CFD Forum

Generating elliptic grid around NACA SC2-0714 airfoil

Register Blogs Community New Posts Updated Threads Search

Like Tree5Likes

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   November 3, 2015, 08:50
Default
  #21
Member
 
mechiebud
Join Date: Jan 2015
Posts: 49
Rep Power: 11
mechiebud is on a distinguished road
Quote:
Originally Posted by naffrancois View Post
Here are some pictures of results of applying different approaches I did some time ago:
- TFI
- Laplace
- Laplace + forcing functions
- Hyperbolic

As you see, the TFI and Laplace without forcing terms give a poor quality grid. The reason is that they do not have any mechanism to enforce orthogonality and much control on the interior grid spacing. With forcing functions you can force the grid to some extend

I think I took as a reference the source codes coming with the book of Blazek:

- Computational fluids dynamics: principles and applications

Attachment 40546

Attachment 40547

Attachment 40548

Attachment 40549
Hi I too am generating elliptic O grid on symmetric airfoil using same method. But as I increase the no of iterations I am getting errors as shown in the image. I have generated initial points using TFI. Can anyone please guide me furthur.
Attached Images
File Type: png export.png (38.3 KB, 57 views)
mechiebud is offline   Reply With Quote

Reply


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
SU2 AOA optimization 454514566@qq.com SU2 9 March 7, 2022 17:17
elliptic grid generation (orthogonal) vasu Main CFD Forum 8 October 28, 2015 16:20
[ICEM] O-grid mesh for NACA airfoil SR-71 ANSYS Meshing & Geometry 0 February 6, 2015 08:45
2D FFD Optimization RLangtry SU2 2 August 5, 2014 10:48
Structured Airfoil Grid Generator A.S. Main CFD Forum 1 September 30, 2008 19:29


All times are GMT -4. The time now is 23:40.