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

Airfoil Analysis

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

LinkBack Thread Tools Display Modes
Old   April 23, 2009, 09:47
Post Solid Airfoil Analysis (Stagnation vs Statitic Temps)
New Member
G. Gilson
Join Date: Apr 2009
Posts: 2
Rep Power: 0
G. Gilson is on a distinguished road
Hi I am modelling a solid airfoil, usig ideal gas equation, mach number = 0.85, second order discretization, sutherland law (for viscosity), viscous heating on.

Now I am interested in the temperatures inside the airfoil, and not on the surface.

I am setting up a single boundary condition -pressure afar, with press =20980 and and angle of attack of 3 and a temp = 216.7 K.

I am getting a result, stating that the inside temperature is = to the stagnant temperature.

I have checked for grid independency, residuals and converge and all seems to be ok.

Has anyone any idea, or come arcoss literature that might confirm my CFD analysis please?

Last edited by G. Gilson; April 23, 2009 at 14:08.
G. Gilson is offline   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
Multi-element airfoil analysis CFD Rookie Main CFD Forum 12 November 17, 2016 07:07
airfoil analysis Hammam CFX 10 June 22, 2007 13:18
Airfoil Mesh for DES Analysis - y+ Value asd Main CFD Forum 1 May 3, 2007 10:13
y+ for Airfoil Analysis asd Main CFD Forum 3 April 18, 2007 10:54
quasi steady analysis of 2d airfoil (pitching) Alex FLUENT 1 February 10, 2006 03:54

All times are GMT -4. The time now is 13:16.