CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > SU2

AoA derivative for NACA0012?

Register Blogs Community New Posts Updated Threads Search

Like Tree2Likes
  • 1 Post By Ry10
  • 1 Post By fpalacios

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   April 15, 2016, 13:53
Default AoA derivative for NACA0012?
  #1
New Member
 
Ryan Barrett
Join Date: May 2015
Posts: 15
Rep Power: 11
Ry10 is on a distinguished road
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!
kmandar likes this.
Ry10 is offline   Reply With Quote

Old   April 22, 2016, 03:15
Default
  #2
Super Moderator
 
Francisco Palacios
Join Date: Jan 2013
Location: Long Beach, CA
Posts: 404
Rep Power: 15
fpalacios is on a distinguished road
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
kmandar likes this.
fpalacios is offline   Reply With Quote

Old   April 28, 2016, 17:57
Default
  #3
New Member
 
Ryan Barrett
Join Date: May 2015
Posts: 15
Rep Power: 11
Ry10 is on a distinguished road
That did the trick. I thought it was in 1/deg not 1/rad. Thanks!
Ry10 is offline   Reply With Quote

Reply

Tags
angle of attack, derivative, su2


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
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


All times are GMT -4. The time now is 12:08.