CFD Online Logo CFD Online URL
Home > Forums > Main CFD Forum

Windtunnel Experiment Data

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

LinkBack Thread Tools Display Modes
Old   March 4, 2000, 06:32
Default Windtunnel Experiment Data
Yap Wen Jiun
Posts: n/a
I am a newcomer in this forum. I don't know this question has been asked before or not.

Where do I get the most accurate or fundamental windtunnel result for an airfoil (such as NACA 23012) so that I can compare to my CFD solutions (using PHOENICS).

For example, at Reynold number of 5 x 10+6, there will be different lift curve for NACA 23012 in different books. So there must be some kind of references. Please tell me.
  Reply With Quote

Old   March 5, 2000, 15:46
Default Re: Windtunnel Experiment Data
Ahmed Al-otaibi
Posts: n/a
You can check in one of the famous books"Wing sections">>

I suggest you using NACA0012 section to validate your code..much more popular and data is available in most of journals and aerodynamics books.. hope you good luck..
  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 can I use this experiment data? turbinesv CFX 2 October 7, 2008 02:21
How to update polyPatchbs localPoints liu OpenFOAM Running, Solving & CFD 6 December 30, 2005 18:27
About low Reynolds number airfoil experiment data. zqnwpu Main CFD Forum 5 December 25, 2004 04:52
Ventilation Simulation & Experiment Data Luo Shengping FLUENT 2 November 30, 2000 05:00
Ventilation Simulation & Experiment Data Luo Shengping Main CFD Forum 2 November 29, 2000 11:29

All times are GMT -4. The time now is 22:26.