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CFD Anderson.. Chapter 10: Supersonic Flow over a Flat plate

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Old   August 14, 2013, 09:34
Default c code
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Quote:
Originally Posted by venkateshaero View Post
if u want similar code in C . i will give u
i also need the code please sent me sreekonchira@gmail.com
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Old   August 21, 2013, 17:31
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can u send me a copy to me at karankumar9931034374@gmail.com
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Old   October 17, 2013, 14:55
Default M25 case for supersonic flow at 200,000ft
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Has anyone done the second case in Anderson CFD book ?

Mach=25
Alt=200,000ft (60km)
L=0.005;

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 ?
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Old   February 11, 2015, 10:44
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Hi,

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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