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

I want NACA0012 simulation datas

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

Like Tree4Likes
  • 1 Post By Santana
  • 1 Post By James Date
  • 2 Post By Frederic Felten

Reply
 
LinkBack Thread Tools Display Modes
Old   December 23, 2004, 09:22
Default I want NACA0012 simulation datas
  #1
Santana
Guest
 
Posts: n/a
Hi.

I hope to simulate NACA0012 airfoil numerically at low Reynolds in laminar flow.

B.C. my code is incompressible code.

So I tried to search some numerical/experimental datas(like Cp, Cl, Cd) of NACA0012 at low Reynolds and laminar flow.

But mainly the reference datas are results of Compressible flow (numerically)at Mach=0.8 or 0.5.

So How to get the reference value of NACA0012 airfoil at low Reynolds in laminar flow ?
rezahasan likes this.
  Reply With Quote

Old   December 23, 2004, 09:33
Default Re: I want NACA0012 simulation datas
  #2
James Date
Guest
 
Posts: n/a
Here's two useful refs for NACA 0012 data:

1) "NACA0012 Airfoil", AGARD Advisory Report, Thibert, J.J. and Grandjacques, M. and Ohman, L.H., 1979.

2) "Low Speed Aerodynamic Characteristics of NACA0012 Airfoil Section, Including the Effects of Upper Surface Roughness Simulation Hoarfrost", National Physical Laboratory (NPL), Gregory, N. and O'Reilly, O.L., 1970, No. 1308.

Regards James
rezahasan likes this.
  Reply With Quote

Old   December 28, 2004, 12:58
Default Re: I want NACA0012 simulation datas
  #3
Frederic Felten
Guest
 
Posts: n/a
Hi there,

1)- Check the following webpage:

http://www.unibas.it/utenti/bonfiglioli/node10.html

It might be useful if you want to validate the viscous terms of your code. There are some velocity profile available.

Keep in mind that these are only numerical results that Bonfiglioli performed.

2)- Also check the following paper: Yu D, Mei R, Shyy W. "A multi-block lattice Boltzmann method for viscous fluid flows". Int. J. Numer. Methods Fluids Vol 39, pp 99120, 2002

They apparently evaluated their numerical scheme by computing the flow around a NACA 0012 for Re=500; 1000, 2000, and 5000.

Again, these are numerical results and not experimental data.

Hope this might help. Good luck

Frederic Felten
rezahasan and hichemgm like this.
  Reply With Quote

Reply

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
Why my simulation not agree with the wind tunnel experiment zhaowei CFX 4 July 11, 2015 03:36
Simulation of a complex wing in solidworks flow simulation niels1900 FloEFD, FloWorks & FloTHERM 6 April 20, 2011 10:44
NACA0012 compressible static simulation paolopaolo88 OpenFOAM 1 April 14, 2011 10:29
GUI crash and simulation engine still running RPJones FLOW-3D 2 November 9, 2010 09:18
velocity profile export from a simulation onto another sudhirlv STAR-CCM+ 1 September 12, 2010 18:57


All times are GMT -4. The time now is 15:58.