|October 17, 2013, 14:55||
M25 case for supersonic flow at 200,000ft
Join Date: May 2013
Posts: 65Rep Power: 4
Has anyone done the second case in Anderson CFD book ?
I tried it and it gives me complex numbers. i used the free stream properties at that altitude.
I used the same 70*70 grid .
should i be missing something ?
|February 11, 2015, 10:44||
Join Date: Feb 2012
Posts: 13Rep Power: 5
I have uploaded a Matlab code that solves the original problem. It can be downloaded from MathWorks here: http://www.mathworks.com/matlabcentr...r-a-flat-plate
Hope this helps!
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