CFD Online Logo CFD Online URL
Home > Forums > FLUENT

Meshing an aerofoil with a plain flap

Register Blogs Members List Search Today's Posts Mark Forums Read

LinkBack Thread Tools Display Modes
Old   November 15, 2005, 15:24
Default Meshing an aerofoil with a plain flap
Posts: n/a
I am trying to mesh an aerofoil with a plain flap in Gambit. Usually when dealing with just an aerofoil the top and bottom edges are splitted at some point to create a non-uniform grid spacing and a uniform grid spacing at some point on the aerofoil. since the aerofoil with flap has a space in between, does this affect it? How does the grid spacing come into account.I modelled it by cutting the aerofoil towards the leading edge and then rotating the leading edge to the desired angle (30degrees)to get the flap.Any advise on how to create the farfield boundary as well?

  Reply With Quote


Thread Tools
Display Modes

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 On
Pingbacks are On
Refbacks are On

Similar Threads
Thread Thread Starter Forum Replies Last Post
[ICEM] 2d Aerofoil meshing in ansys ICEM syler3321 ANSYS Meshing & Geometry 2 February 3, 2012 02:59
Aerofoil meshing eugene Main CFD Forum 1 September 7, 2008 00:11
Meshing aerofoil Sajal Sengupta FLUENT 0 June 19, 2006 05:08
digitizing an aerofoil/ meshing problems Simon FLUENT 2 February 27, 2006 12:18
Meshing An airfoil with a simple plain flap S. Kalam FLUENT 7 January 30, 2005 21:22

All times are GMT -4. The time now is 18:22.