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

Cp for NACA0012, angle of attack=14degree

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

LinkBack Thread Tools Display Modes
Old   October 29, 2008, 06:38
Default Cp for NACA0012, angle of attack=14degree
Posts: n/a
Nowdays, I have calculate a flow for NACA0012 airfoil. The freestream velocity is 30m/s. The angle of attack is 14 degree. In our code, we use a RANS S-A mode with DES. The Cp curve can get from following I am not sure whether the results are right. Who can help me analysis the results? Thank you!

Of couse, if someone has the experimental data or CFD results for this case or other case (angle of attack =15,16,18,... ), and can send to me, i will be very thankful. My email:

Thank you!!
  Reply With Quote

Old   October 29, 2008, 23:12
Default Re: Cp for NACA0012, angle of attack=14degree
Posts: n/a
Here, Re=1.0e+6
  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
InterFoam contact angle JoaoMiranda OpenFOAM Running, Solving & CFD 7 October 20, 2016 06:27
Import netgen mesh to OpenFOAM hsieh Open Source Meshers: Gmsh, Netgen, CGNS, ... 32 September 13, 2011 05:50
Normal vector, slope and aspect angle g_niro Main CFD Forum 0 February 2, 2011 18:24
Theoretical background of formula for dynamic contact angle in interfoam sebastian_vogl OpenFOAM Running, Solving & CFD 3 June 22, 2009 12:25
angle of attack kiran FLUENT 0 September 10, 2004 08:18

All times are GMT -4. The time now is 14:49.