|
[Sponsors] |
January 22, 2013, 06:49 |
NACA 2408 Comparative results.
|
#1 |
New Member
Sárán Greene
Join Date: Nov 2012
Location: Dublin
Posts: 13
Rep Power: 14 |
I'm currently running some simulations on an NACA 2408 airfoil for my final year project. I'm looking at incompressible flow and the main forces I'm concerned with are Lift and Drag. However, I haven't been able to find any published data for an NACA 2408 airfoil or hydrofoil. Does anyone know where I might be able to find any? This may be a silly question but would I be able to use published data from say a 2412 foil and compare it to the results obtained through the simulation? I'm running simulations and, while the graphs for Lift and Drag look ok to me, I've very little experience with CFD so they could be completely wrong.
Thanks in advance. |
|
January 22, 2013, 10:42 |
|
#2 |
Member
venki
Join Date: May 2011
Posts: 84
Rep Power: 15 |
Refer theory of wing section book by abbott
|
|
January 22, 2013, 10:44 |
|
#3 |
Member
venki
Join Date: May 2011
Posts: 84
Rep Power: 15 |
||
January 22, 2013, 11:05 |
|
#4 |
New Member
Sárán Greene
Join Date: Nov 2012
Location: Dublin
Posts: 13
Rep Power: 14 |
Thank you for the reply. I just ordered that book there a few minutes ago.Thanks again.
|
|
January 22, 2013, 13:44 |
|
#5 |
Member
venki
Join Date: May 2011
Posts: 84
Rep Power: 15 |
k fine.I have soft copy of that book.
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Problem: Very long "write" time (~2h-3h) for results and transient results | Shawn_A | CFX | 16 | April 12, 2016 21:49 |
Transient Run - Output "Time" in partial results? | evcelica | CFX | 2 | May 16, 2012 22:36 |
Search for cd and cl experimental results of NACA 0012 | spk | Main CFD Forum | 3 | April 17, 2012 15:28 |
Lost Scenario Results..?? | Fugacity | Autodesk Simulation CFD | 1 | February 24, 2012 11:48 |
Problems with repeating results | Lee | Siemens | 4 | May 26, 2006 04:39 |