CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS > FLUENT

Simulation NACA 0018, Cl, Cm, Cd

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

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   June 8, 2022, 15:44
Smile Simulation NACA 0018, Cl, Cm, Cd
  #1
New Member
 
Vyacheslav Papkov
Join Date: May 2022
Posts: 4
Rep Power: 2
ChRiZZ is on a distinguished road
Hello! I am modeling the aerodynamic profile of a NACA 0018 wing in a 2d formulation of the problem. I have an error when getting Sd and Sf in +- 0.15. For example, if I have a theoretical value of +-0.6 at an angle of attack of 16 degrees, then my result is 0.45. How can this be fixed? SST turbulence model, screenshots attached below
ChRiZZ is offline   Reply With Quote

Reply

Tags
airfoil 2d, airfoil mesh, help me, mesh 2d, naca 0018

Thread Tools Search this Thread
Search this Thread:

Advanced Search
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 Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
NACA 0012 Winglet Project: need guidance setting up simulation at subsonic speeds Rarepepe FLUENT 1 October 17, 2015 22:24
restarting paused transient simulation using reactingFoam JMDag2004 OpenFOAM Running, Solving & CFD 1 August 10, 2015 11:15
NACA 2412 airfoil simulation using Turbulence Models mahbub03 Main CFD Forum 0 February 1, 2011 13:48
NACA 0018 Experimental Data andygir Main CFD Forum 1 October 15, 2010 13:03
NACA 0012 simulation results Luis FLUENT 3 February 15, 2006 12:42


All times are GMT -4. The time now is 08:22.