 |
 |
 |
|
|
|
[Sponsors] | ||||
March 24, 2007, 10:18
|
analyzing NACA 0012 airfoil
|
#1 |
|
Guest
Posts: n/a
|
Hi everybody! i would like to analyze the NACA 0012 airfoil to determine the lift and drag coefficients at different angle of attack by using cfx. can you please tell me the steps required to achieve that.
thanks M.Hammam. |
|
|
||
|
May 2, 2007, 05:19
|
Re: analyzing NACA 0012 airfoil
|
#2 |
|
Guest
Posts: n/a
|
Hello I am an aerospace engeneering and want to NACA 0012 airfoil codes to determine the pressure,lift and drag coefficients at different angle of attack by using cfx. thanks N.Tohidi
|
|
|
|
||
|
May 3, 2007, 12:07
|
Re: analyzing NACA 0012 airfoil
|
#3 |
|
Guest
Posts: n/a
|
What do you mean with "codes" ??
The (x,y) coordinates that define the contour of the airfoil? Santiago. |
|
|
|
||
|
May 3, 2007, 12:17
|
Re: analyzing NACA 0012 airfoil
|
#4 |
|
Guest
Posts: n/a
|
This is really breaking news.
Good luck, Gert-Jan |
|
|
|
||
|
May 7, 2007, 04:47
|
Re: analyzing NACA 0012 airfoil
|
#5 |
|
Guest
Posts: n/a
|
Choose "The Applet" on http://www.mh-aerotools.de/airfoils/javafoil.htm to run JAVAFOIL. Why bother with CFD...
|
|
|
|
||
|
May 14, 2007, 10:30
|
Re: analyzing NACA 0012 airfoil
|
#6 |
|
Guest
Posts: n/a
|
Hello I require analyzing NACA 0012 airfoil. Thanks
|
|
|
|
||
 |
| Thread Tools | |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| NACA 0012 AIRFOIL | naveen | OpenFOAM Other Meshers: ICEM, Star, Ansys, Pointwise, GridPro, Ansa, ... | 7 | April 14, 2011 11:03 |
| problem with stall in naca 0012 airfoil | thanos | FLUENT | 0 | February 18, 2010 11:36 |
| Laminar flow past oscillating Naca 0012 airfoil | kafkaf | Main CFD Forum | 1 | April 7, 2009 02:49 |
| Solving naca 0012 airfoil | naveen | OpenFOAM Pre-Processing | 3 | February 17, 2009 09:25 |
| Drag predicion for a NACA 0012 airfoil | Peter Giannakopoulos | FLUENT | 7 | March 9, 2004 15:32 |
Linear Mode
