CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > General Forums > Main CFD Forum

Taylor Maccoll Eq. with Runge Kutta

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   November 21, 2015, 22:31
Default Taylor Maccoll Eq. with Runge Kutta
  #1
yow
New Member
 
Yang
Join Date: Jun 2015
Posts: 25
Rep Power: 10
yow is on a distinguished road
Before I go use CFD, I wanted to approximate the supersonic flow field after a shock in front of a cone (0 deg. angle of attack). I used 4th order Runge Kutta with Taylor Maccoll eq. and am getting Vtheta = 0 at 31 deg cone half angle when I assume my shock beta = 34 deg. I've stared at my code for 20 h and have manually coded the Runge Kutta eq. as well as using ode45 function and get the same results. My step size is - .001. Can anyone please help? Maybe I'm just braindead...

Apologies if this is the wrong place to ask.
yow is offline   Reply With Quote

Old   December 6, 2015, 11:22
Default
  #2
yow
New Member
 
Yang
Join Date: Jun 2015
Posts: 25
Rep Power: 10
yow is on a distinguished road
Nevermind, I found the answer after contemplating for a while... The initial Vtheta used for the Taylor-Maccoll equations must be negative to account for the decreasing Vr due to the flow relieving effect of the 3D cone surface.
yow is offline   Reply With Quote

Old   April 29, 2021, 14:12
Default Similar Issue
  #3
New Member
 
Join Date: Apr 2021
Posts: 1
Rep Power: 0
psakkos is on a distinguished road
I am having a similar issue. My RK4 is approximating a very high cone angle that is very close to the shock. What did you code your program in? I’m using Matlab. My initial conditions are right, though, so I don’t know what the issue is
psakkos is offline   Reply With Quote

Reply

Tags
matlab code, quasi-2d, runge-kutta, taylor maccoll


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
Main advantage of using Runge Kutta of higher order? jakubstary Main CFD Forum 14 August 20, 2019 16:15
rhoCentralFoam Runge Kutta Henning86 OpenFOAM Running, Solving & CFD 24 December 13, 2016 10:12
1D Burgers euqation with 4th Runge Kutta dokeun Main CFD Forum 3 August 8, 2011 06:34
Runge Kutta Optimization vasanth Main CFD Forum 6 December 2, 2005 13:07
Diagonally Dominate Runge Kutta Method Anthony Iannetti Main CFD Forum 0 January 23, 2001 21:27


All times are GMT -4. The time now is 07:30.