CFD Online Logo CFD Online URL
Home > Forums > OpenFOAM

Generating Mesh for Body-Tail missile configuration using OF

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

LinkBack Thread Tools Display Modes
Old   April 19, 2010, 06:14
Question Generating Mesh for Body-Tail missile configuration using OF
Senior Member
Join Date: Oct 2009
Location: Chennai, India
Posts: 102
Rep Power: 10
mecbe2002 is on a distinguished road
Hi all,

I am in the process of generating mesh for a Body-Tail missile configuration using "blockMesh" tool. I find it difficult to mesh around the conical part of the missile. (Plz ref the attached file for the drawing). Is is possible to have pure hex mesh through out the domain

Any suggestions for this.

Attached Images
File Type: jpg vertex.jpg (21.1 KB, 31 views)
Attached Files
File Type: pdf body-wing(2D).pdf (5.7 KB, 34 views)
File Type: pdf automesh.pdf (8.8 KB, 34 views)
mecbe2002 is offline   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
SnappyHexMesh for internal Flow vishwa OpenFOAM Native Meshers: snappyHexMesh and Others 24 June 27, 2016 08:54
[ICEM] Hexa mesh, curve mesh setup, bunching law Anorky ANSYS Meshing & Geometry 4 November 12, 2014 01:27
Moving mesh Niklas Wikstrom (Wikstrom) OpenFOAM Running, Solving & CFD 122 June 15, 2014 06:20
Dynamic moving mesh Pei-Ying Hsieh (Hsieh) OpenFOAM Running, Solving & CFD 64 June 7, 2012 10:04
unstructured vs. structured grids Frank Muldoon Main CFD Forum 1 January 5, 1999 11:09

All times are GMT -4. The time now is 14:54.