Home > Forums > Software User Forums > SU2

SU2 additional input boundary field

Updated Threads

Reply

Search this Thread

November 17, 2016, 03:37	SU2 additional input boundary field	#1
martinsimon New Member Martin Simon Join Date: Feb 2015 Posts: 5 Rep Power: 11	Hello guys! I am researching advantages of applying air jets to enhance wing/blade performance. Similar to this: http://www.scer.rpi.edu/cefpac/wp-co...d-2_Page_4.jpg Is there a way to produce such an analysis on SU2? (e.g create a boundary face like in OpenFOAM) I have come across many others who have been struggling with this question, but no answers yet. :/ Thank You!

Reply

Tags

aerodynamics, blade, su2, synthetic jet, wing

« Previous Thread | Next Thread »

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 Forum Rules

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
Centrifugal fan	j0hnny	CFX	13	October 1, 2019 13:55
[Other] dynamicTopoFVMesh and pointDisplacement	RandomUser	OpenFOAM Meshing & Mesh Conversion	6	April 26, 2018 07:30
Waterwheel shaped turbine inside a pipe simulation problem	mshahed91	CFX	3	January 10, 2015 11:19
Difficulty In Setting Boundary Conditions	Moinul Haque	CFX	4	November 25, 2014 17:30
RPM in Wind Turbine	Pankaj	CFX	9	November 23, 2009 04:05

All times are GMT -4. The time now is 17:36.