CFD Online Logo CFD Online URL
Home > Forums > Software User Forums > SU2

Boundary Layer Thickness Extraction

Register Blogs Members List Search Today's Posts Mark Forums Read

LinkBack Thread Tools Search this Thread Display Modes
Old   July 25, 2019, 12:07
Default Boundary Layer Thickness Extraction
New Member
Shubham jhamb
Join Date: Jan 2018
Posts: 3
Rep Power: 8
Shubham_J is on a distinguished road
I am using SU2 as a tool to analyze flow over an airfoil in supersonic regime. I wanted to compute the boundary layer thickness over the airfoil. I presume it changes over the entire blade surface due to the contouring of the airfoil.

Is there any way I can calculate the boundary layer thickness over the airfoil using TecPlot and flow.dat from the simulation?

Any insight will be helpful.

Shubham_J is offline   Reply With Quote


Thread Tools Search this Thread
Search this Thread:

Advanced Search
Display Modes

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
My radial inflow turbine Abo Anas CFX 27 May 11, 2018 01:44
CFD analaysis of Pelton turbine amodpanthee CFX 31 April 19, 2018 18:02
Basic Nozzle-Expander Design karmavatar CFX 20 March 20, 2016 08:44
Questions about Boundary Layer Thickness and Turbulence Models famerfamer STAR-CCM+ 3 July 12, 2012 09:47
boundary layer thickness 98.4F Main CFD Forum 1 December 29, 2000 07:23

All times are GMT -4. The time now is 01:06.