|
[Sponsors] |
April 15, 2016, 13:53 |
AoA derivative for NACA0012?
|
#1 |
New Member
Ryan Barrett
Join Date: May 2015
Posts: 15
Rep Power: 11 |
I want to find the adjoint derivative of drag with respect to AoA for the NACA0012. I found the Sens_AoA in the history.csv file when I run the ADJOINT using the QuickStart files. But when I do finite difference this value is not even close to what the finite differences says the derivative should be. Is this the way to get the AoA derivative or is there a better way? There are lots of design variables available but I can't figure out a way to get the derivative of angle of attack.
Thanks! |
|
April 22, 2016, 03:15 |
|
#2 |
Super Moderator
Francisco Palacios
Join Date: Jan 2013
Location: Long Beach, CA
Posts: 404
Rep Power: 15 |
Hi,
I'm using the sensitivity with respect to the AoA and the error compared with FD is acceptable. Are you sure that you are using 1/rads or 1/deg in both numbers? as you know, the factor is 57.2957795131. as far I remember Sens_AoA uses 1/rads Best Regards, Francisco Palacios |
|
April 28, 2016, 17:57 |
|
#3 |
New Member
Ryan Barrett
Join Date: May 2015
Posts: 15
Rep Power: 11 |
That did the trick. I thought it was in 1/deg not 1/rad. Thanks!
|
|
Tags |
angle of attack, derivative, su2 |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Pitching Airfoil: Cd Vs AOA | mooby | FLUENT | 0 | June 19, 2015 03:43 |
Simulating flow past airfoil with different AOA | ramin | FLUENT | 4 | April 22, 2015 14:09 |
Derivative of a scalar or a variable through UDF | fevi84 | Fluent UDF and Scheme Programming | 7 | February 3, 2015 22:39 |
discontinuous second derivative | new_at_this | Main CFD Forum | 9 | April 28, 2012 17:55 |
Simulating flow past airfoil with different AOA | Quarkz | Main CFD Forum | 2 | January 6, 2006 11:56 |