CFD Online Logo CFD Online URL
Home > Forums > Software User Forums > ANSYS > FLUENT

NACA 0009

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

LinkBack Thread Tools Display Modes
Old   July 23, 2004, 16:28
Default NACA 0009
Posts: n/a
Hi, Im newbie on this forum, and I don`t write very good the English Language,so Im sorry for my gramatical mistkes. Well, I`m trying to simulate a flow over an airfoil, with ICEM profile, but I don`t Know How I can generate thid *.msh profile, Thanks.
  Reply With Quote

Old   July 23, 2004, 16:50
Default Re: NACA 0009
Posts: n/a
Im Sorry, Im wrong the ICEM profile that I must import is *.data or similar, and the h=0.06*c; p=0.5*c; c=0.2 for my aifoil.
  Reply With Quote

Old   August 17, 2004, 14:18
Default Re: NACA 0009
Posts: n/a
Hola Raul......

No eniendo bien tu problema.....supongo que tienes las coordenadas del perfil en tu archivo *.dat ......quer quieres hacer con ellas....pasarlas directamente a *.msh....???

I supossed you have the coordinates of your airfoil in a *.dat format .....what dou you want to do with them ???
  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
How to import NACA 0012 Profile in Gridgen maplepink Main CFD Forum 17 May 7, 2013 13:01
Mismatched NACA profiles xTamx420 Main CFD Forum 0 July 7, 2011 10:11
Symmetric NACA Airfoil Lift and Drag Data jrider22 Main CFD Forum 3 April 15, 2010 04:59
Ansys CFX Vs. NACA Summary Report. Mismatch Result Santiago Orrego. CFX 3 February 5, 2007 13:05
NACA 0012 simulation results Luis FLUENT 3 February 15, 2006 12:42

All times are GMT -4. The time now is 08:39.